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Soyuz rocket launches the Aist-2T pair, Iranian satellites

A Soyuz-2-1b/Fregat rocket closed Russia's orbital launch attempts in 2025 with a mission delivering a pair of Aist-2T Earth imagers and 50 hitchhiking payloads, including a trio of Iranian satellites, on December 28.


launch

Aist-2T mission at a glance:

Launch date and time
2025 Dec. 28, 16:18:05.462 Moscow Time
Spacecraft mass 670 kilograms
Projected life span
No less than 5 years
Aist-2T dimensions 2.2 x 1.3 x 2.7 meters
Aist-2T panchromatic resolution 1.6 meters (in nadir); 1.9 meters (stereo)
Aist-2T multi-spectral resolution 4.8 meters (in nadir); 5.9 meters (stereo)
Aist-2T imaging data downlink capacity
1,600 megabits per second
Spacecraft prime developer
RKTs Progress
Launch vehicle
Soyuz-2-1b/Fregat No. 142-602
Payload fairing
81KS No. A15000-071
Launch site
Target orbit 550-kilometer Sun-synchronous
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Aist

The dual-purpose Aist-2T satellite with a mass of 670 kilograms, was developed at RKTs Progress in Samara under a 2019 contract with the Roskosmos State Corporation, which ordered a two-spacecraft system producing stereo-imaging of the Earth surface from a Sun-synchronous orbit. The stereo imagery would be possible thanks to a dual set of cameras on each Aist-2T (instead of one on the previous-generation Aist-2D, launched in 2016, making it possible to photograph each area under a slightly different angle.

The Aist-2T satellite was reported to be capable of capturing images with a resolution as high as 1.6 meters, when photographing in nadir (directly below its flight path) in pan-chromatic mode. In the same imaging mode, it could also produce stereo images with a resolution up to 1.9 meters. Multi-spectral and color imagery was reported to be possible with a resolution of 4.8 meters when pointing in nadir or up to 5.9 meters for stereo sets of photos.

The Aist-2T variant also featured a built-in propulsion system for the first time, while the satellite's downlink channel for sending imaging data back to Earth was expanded from 150 megabits per second on Aist-2D to 1,600 megabits per second on the 2T version.

As of February 2020, the Aist-2T pair was scheduled for launch in November 2022, but by 2021, it slipped to 2023 and was later re-scheduled for Dec. 25, 2024. By mid-October 2024, the mission was postponed again, until at least March 17, 2025, and by the end of 2024, it was rumored to be delayed until June 26, 2025. Early in 2025, the launch slipped to the end of August 2025 and, ultimately to December of the same year.

Secondary payloads

image

In addition to the launch of the Aist-2T pair, the same Soyuz-2-1b rocket was also booked to carry 50 dual-purpose secondary payloads, ranging from light-weight experimental satellites down to an assortment of educational cubesats and a small carrier platform, itself designed to release the tiniest satellites known as pikosats. A total of 33 payloads were to be deployed from 17 launch containers provided by Moscow-based Aerospeis Kapital.

The most notable secondary payloads on the mission were two Marafon-IoT experimental satellites (INSIDER CONTENT), developed at ISS Reshetnev and intended for paving the way to the so-called Internet-of-Things satellite system, however, by the time they reached the launch pad, the main project was facing cancellation due shrinking Russian space budget.

The most significant foreign payload on the Aist-2T mission was a trio of Iranian dual-purpose satellites all intended for remote-sensing of the Earth's surface. Other small foreign payloads were ordered by various institutions in Montenegro, Kuwait, Qatar, Ecuador and Belarus.

Also, the St. Petersburg-based STTs government-supported center reported sending a total of eight small payloads on the Aist-2T mission.

The payload fairing of the rocket also carried a logo of the Pixidex company from South Africa, which specialized in equipment for suppressing drones, but it was not immediately clear which satellite carried its payload.

pad

Payloads aboard the Soyuz launch on Dec. 28, 2025:

 

Spacecraft

Mass, kg

Developer/Operator

Mission/Type

1

Aist-2T No. 1

670

RKTs Progress/Roskosmos

Remote-sensing (primary payload)

2 Aist-2T No. 2
670
RKTs Progress/Roskosmos
Remote-sensing (primary payload)
3 Aist-ST
27.75
STTs, Samara Aerospace University/Space-PI
Remote-sensing 16U cubesat
4 Ansat-1
?
STTs
3U cubesat for optical imaging
5 Argus-312
?
NPO Kaisat/Germes Experiments with drone control(?)
6 Grifon No. 1
?
Novosibirsk State University
16U cubesat
7 Grifon No. 2
?
Novosibirsk State University
16U cubesat
8 Grifon No. 3
?
Novosibirsk State University
16U cubesat
9 Grifon No. 4
?
Novosibirsk State University
16U cubesat
10 DCS-1
?
Sputniks/Tunisia
1U cubesat
11 Eya-2
?
NPO Kaisat/Germes  
12 Khors No. 5
?
KB ProKIT/Bauman Technical University
8U cubesat within UniverSat program
13 Kowsar-1.5 (2See-1)
?
Iran
Remote sensing
14 Lobachevsky (IC)
26.7
Geoskan
Remote-sensing 16U cubesat
15 Luca
?
Sputniks for Montenegro
1U cubesat
16 Marafon No. 1 (IC)
~100
ISS Reshetnev
IoT (Experimental)
17 Marafon GVM mockup
~100
ISS Reshetnev
IoT (Mass simulator)
18 NASBSat-1
?
Sputniks/Belarus
6U cubesat
19 NASBSat-2
?
Sputniks/Belarus
6U cubesat
20 Mokha-1
?
NPO Kaisat/Germes
 
21 MorSat-1
?
NILAKT, Siberian Aerospace University
6U cubesat within UniverSat program
22 Mule-4T
?
RuVDS, OKB-5
Sub-satellite carrier for RuVDSat
23 Paya (Tolou-3)
50
Iran
Remote sensing spacecraft 1.2 x 1 x 1 m. in size
24 Polytech Universe-6
25
STTs, St. Petersburg Polytech
16U cubesat for electromagnetic measurements
25 QMR-KWT-2
?
Sputniks for Kuwait
6U cubesat
26 SakhaCube-Cholbon
1.211
Sputniks, Academy of Sciences at Sakha Republic
1U cubesat
27 SCH-619
?
STTs
3U cubesat for electromagnetic measurements
28 SITRO-AIS-57
?
Sputniks, Sitronics Group
Automated identification of vessels
29 SITRO-AIS-58
?
Sputniks
 
30 SITRO-AIS-59
?
Sputniks
 
31 SITRO-AIS-60
?
Sputniks
 
32 SITRO-AIS-61
?
Sputniks
 
33 SITRO-AIS-62
?
Sputniks
 
34 SITRO-AIS-63
?
Sputniks
 
35 SITRO-AIS-64
?
Sputniks
 
36 SITRO-AIS-65
?
Sputniks
 
37 SITRO-TD-3
?
Sputniks
3U cubesat
38 SITRO-TD-4
?
Sputniks
3U cubesat
39 Skorpion (Sozvezdie-270)
25
NIIYaF MGU, NILAKT DOSAAF
16U cubesat with gamma ray bursts and transient source detectors
40 SM-3.1
?
STTs  
41 TriSat-1
0.5
AO OKB-5
Pico-satellite
42 TriSat-2 (RUVDSSat-1)
0.5
AO OKB-5
Pico-satellite
43 TriSat-3 (QUbeSat-1)
0.5
AO OKB-5
Pico-satellite for University of Qatar
44 TriSat-4
0.5
AO OKB-5
Pico-satellite
45 TsSTP-3.10
?
STTs
16U cubesat
46 UTE-Galapagos
?
Equador
?
47 Vladivostok-2 (TsSTP-3.11
?
STTs
8U cubesat within the UniverSat program
48 VM-3.1
?
STTs
?
49 Zafar-2
113
Iran
Remote sensing
50 Zorky-2M VPE
24
Sputniks 12U cubesat
51 Zorky-2M No. 5
24
Sputniks 12U cubesat
52 Zorky-2M No. 7
24
Sputniks 12U cubesat

Launch campaign

fregat

The Soyuz launch vehicle for the Aist-2T mission was delivered by rail from Samara to Vostochny in mid-November 2024.

On Oct. 31, 2025, Roskosmos announced the start of work with the Fregat upper stage for the Aist-2T mission in Vostochny. The space tug was extracted from its transport container and placed at its work site inside the spacecraft processing building for upcoming pneumatic and electric tests. Upon their completion, the stage was to be ready for delivery to the fueling station, ZNS, for propellant and pressurized gases loading, which would represent irreversible operations and kick off the active launch campaign, but at the time, Roskosmos did not mention the launch date for the mission.

According to unofficial sources, by early November 2025, the industry committed to launching the mission on Dec. 28, 2025. The electric and pneumatic-vacuum tests of the Fregat upper stage were completed by Nov. 20, 2025, and the space tug was reported sent to fueling with propellant and pressurized gases.

The critical meeting of the State Commission overseeing the launch was scheduled for Dec. 5, 2025, and it apparently confirmed the readiness of the mission for Dec. 28, 2025, launch. On Dec. 8, 2025, Roskosmos reported ongoing assembly of booster stages for the Soyuz-2.1b rocket, secondary payloads and the main payload section for the mission in Vostochny. The state corporation also confirmed the completion of Fregat fueling operations but still did not mention the planned launch date for the mission.

The integration of the four boosters of the first stage with the core booster of the second stage was reported completed on Dec. 11, 2025. An Il-76 transport aircraft with a pair of Aist satellites landed at Vostochny's airport on Dec. 15, 2025.

By Dec. 23, 2025, the assembly of the payload section was completed and it was encapsulated under the 81KS payload fairing of the Soyuz rocket. The next day, the payload section was transferred to the Vehicle Assembly Building, MIK RN, where it was integrated with the third stage of the Soyuz launch vehicle, which in turn was connected to the booster stages of the rocket, completing the assembly of the vehicle. The next day, the State Commission overseeing the launch cleared the vehicle for the rollout to the launch pad, which proceeded as planned on the morning local time in Vostochny on Dec. 26, 2025.

Launch profile

ascent

A Soyuz-2.1b rocket carrying the Aist-2T pair and secondary payloads lifted off from Site 1S in Vostochny on Dec. 28, 2025, at 16:18:05.462 Moscow Time (8:18 a.m. EST).

After a few seconds of vertical ascent under the power of the four boosters of the first stage and the core booster of the second stage, the rocket headed northwest across eastern Russia, aligning its trajectory with a near-polar orbit inclined around 98.57 degrees toward the Equator and an azimuth of 344.13 degrees. The strap-on boosters of the first stage should separated 1 minute 59 seconds after liftoff (Launch+118.9 seconds) in order to crash at Drop Zone No. 981 in the Amurskaya Oblast (Amur Region) on the border between the Tynda and Zeya Districts.

The fairing protecting the payload then split in two halves and separated during the operation of the second stage at 3 minutes 48 seconds in flight (L+228.4 seconds). As a result, the payload fairing fragments should have fallen at Drop Zone No. 983 in the Aldan District in the Sakha (Yakut) Republic.

Moments before the second stage completed its firing 4 minutes and 48 seconds into the flight, the RD-0124 engine of the third stage began to fire through the inter-stage lattice structure, which moments later separated along with the second stage 4 minutes and 48 seconds after liftoff (L+287.9 seconds). Just 1.5 seconds later (L+291.8 seconds), the tail section on the third stage split into three segments. Both, the second-stage booster and the segments of the tail section were to impact the ground at Drop Zone No. 985, in the Vilyusk District, located farther north in the Sakha Republic.

The third stage continued firing, inserting the Fregat upper stage and its passengers into an orbit with an apogee (highest point) of 196 kilometers and a perigee of just 12 kilometers or well in the dense atmosphere. As a result, after its engine cutoff and separation from Fregat, 9 minutes 24 seconds after liftoff (L+563.7 seconds), the third stage began a long free fall back to Earth over the Arctic and Northern Atlantic Oceans. Its trajectory was designed to bring the flaming debris of the booster crashing into the Atlantic Ocean.

Space tug flight profile

Following its split from the third stage at 16:27 Moscow Time, the Fregat was programmed to fire its engine over the Arctic Region 9 minutes 29 seconds after liftoff for around 1.5 minutes to ensure its insertion into a transfer orbit. The stack then climbed passively for around 46 minutes before Fregat fired for the second time near the apogee of its initial orbit, this time over the Antarctica, around 59 minutes 40 seconds after liftoff. The maneuver, lasting less than a minute, inserted the vehicle into a nearly circular orbit around 830 kilometers above the Earth's surface. The primary payload — a pair of Aist-2T satellites — ejected from Fregat's payload adapter, completing the main task of the mission 1 hour 4 minutes and 18 seconds after liftoff.

Roskosmos confirmed the successful release of the Aist-2T satellites slightly more than an hour after the liftoff, adding that the deployment of 50 secondary payloads was ongoing.

According to the flight plan, a total of 48 secondary payloads were to be released in the second target orbit formed by the Fregat upper stage, followed by an additional space tug maneuvers to enter the third target orbit for the deployment of the two Marafon-IoT experimental satellites (INSIDER CONTENT).

The STTs center, which launched eight of its small satellites with the Aist-2T mission, later reported that the command to release its first payload was issued 2.5 hours after the launch and was followed by the commands to deploy its subsequent satellites in next nine minutes:

Moscow Time Payload
18:48:15 TsSTP-3.10
18:51:55 PU-6
18:52:25 TsSTP-3.11
18:55:25 VM-3.1
18:55:55 SCH-619
18:56:25 Ansat-1
18:56:55 SM-3.1
18:57:25 Aist-ST

The company also said that its first communications session with all eight of its payloads took place at 19:23:01 Moscow Time on Dec. 28, 2025.

Before the end of Dec. 28, 2025, Roskosmos confirmed the successful separation of secondary payloads in multiple groups, including a Zorky-2M dual-use imaging satellite.

After the release of its final passenger around five hours after its liftoff from Vostochny, the Fregat was expected to conduct another pre-programmed maneuver to place itself on a reentry trajectory into the Earth's atmosphere and disintegrate over the Equatorial region in the eastern section of the Pacific Ocean.

Around Jan. 5, 2026, the Iranian source Isna.ir reported that "as a result of a problem that arose during the orbital injection of the Paya satellite by the launch vehicle, significant focus was placed on stabilizing the satellite, and required corrective actions were executed with great accuracy." The spacecraft was reported successfully dielivering its first image by Jan. 6, 2026.

By Jan. 8, 2026, the US Space Force cataloged 50 objects in an orbit with an inclination of around 97 degrees:

NORAD ID
Object ID
Epoch
Inclination
Period
Apogee
Perigee
67248
2025-313A 2026-01-08T12:33:23.824224 97.56 98.18 869 473.7
67249
2025-313B 2026-01-08T13:04:42.598272 97.53 97.75 860.3 441.8
67250
2025-313C 2026-01-08T12:44:16.271232 97.64 97.01 729.6 501
67251
2025-313D 2026-01-08T11:57:32.643072 97.59 96.73 708.3 495.7
67252
2025-313E 2026-01-08T11:06:59.334336 97.41 94.64 508.5 493.9
67253
2025-313F 2026-01-08T13:17:20.723712 97.1 92.05 381.6 368
67254
2025-313G 2026-01-08T13:17:52.151712 97.1 92.05 382 368.1
67255
2025-313H 2026-01-08T12:49:57.363744 97.31 95.86 623.1 497.5
67256
2025-313J 2026-01-07T19:37:11.178336 97.41 94.75 517.9 495.4
67257
2025-313K 2026-01-08T11:24:53.418528 97.41 94.75 517.6 495.4
67258
2025-313L 2026-01-08T11:24:38.876544 97.41 94.75 517.5 495.3
67259
2025-313M 2026-01-08T11:22:29.538336 97.42 94.73 516.1 495.1
67260
2025-313N 2026-01-08T03:29:09.094560 97.41 94.74 516.6 495.5
67261
2025-313P 2026-01-08T11:21:41.447232 97.42 94.72 515.6 494.7
67262
2025-313Q 2026-01-08T12:57:03.249216 97.41 94.73 516 495.2
67263
2025-313R 2026-01-07T16:24:49.716000 97.41 94.74 516.1 495.4
67264
2025-313S 2026-01-08T12:57:35.756352 97.42 94.74 516.3 495.6
67265
2025-313T 2026-01-08T11:22:02.391456 97.41 94.73 515.9 495.3
67266
2025-313U 2026-01-08T11:22:00.664320 97.41 94.73 515.9 495.3
67267
2025-313V 2026-01-08T12:56:31.151616 97.41 94.73 515.2 495.7
67268
2025-313W 2026-01-08T12:56:54.166848 97.41 94.73 516.1 495.3
67269
2025-313X 2026-01-08T12:56:23.974368 97.41 94.73 515.6 495
67270
2025-313Y 2026-01-08T12:57:06.465024 97.41 94.73 516 495.3
67271
2025-313Z 2026-01-08T12:57:21.299904 97.41 94.74 516.3 495.6
67272
2025-313AA 2026-01-08T12:55:56.284032 97.41 94.72 515.4 495
67273
2025-313AB 2026-01-08T12:57:07.195968 97.41 94.74 515.6 496.4
67274
2025-313AC 2026-01-08T12:56:25.024992 97.41 94.73 515.7 495.5
67275
2025-313AD D 2026-01-08T11:21:05.236128 97.41 94.73 515 495.8
67276
2025-313AE 2026-01-08T11:21:02.788416 97.41 94.73 515 495.9
67277
2025-313AF 2026-01-08T14:30:45.039744 97.41 94.73 515 496
67278
2025-313AG G 2026-01-08T11:21:02.042784 97.41 94.73 515 495.9
67279
2025-313AH H 2026-01-08T11:20:35.960352 97.41 94.73 515.2 495.4
67280
2025-313AJ 2026-01-08T12:51:39.552480 97.42 94.71 513.5 495.2
67281
2025-313AK 2026-01-08T12:50:43.474560 97.41 94.7 512.3 495.8
67282
2025-313AL 2026-01-08T12:47:01.563936 97.41 94.68 510.3 495.5
67283
2025-313AM M 2026-01-08T11:11:49.918272 97.41 94.67 510 495.3
67284
2025-313AN N 2026-01-08T12:46:56.379936 97.41 94.68 510.3 495.6
67285
2025-313AP 2026-01-08T12:45:48.150720 97.41 94.67 509.5 495.3
67286
2025-313AQQ 2026-01-08T12:45:13.814496 97.41 94.66 509.2 495.4
67287
2025-313AR 2026-01-07T11:29:19.387104 97.41 94.66 508.9 495.4
67288
2025-313AS 2026-01-08T12:45:16.449696 97.41 94.67 510.5 494.3
67289
2025-313AT 2026-01-08T12:44:12.956928 97.41 94.65 508.6 494.9
67290
2025-313AU 2026-01-08 97.41 94.66 508.5 495.2
67291
2025-313AV 2026-01-08 97.41 94.65 508.3 495.1
67292
2025-313AW 2026-01-08 97.41 94.65 508 495.1
67293
2025-313AX 2026-01-08 97.41 94.66 509.7 494.3
67294
2025-313AY 2026-01-08 97.41 94.65 507.8 495.1
67295
2025-313AZ 2026-01-08 97.41 94.65 508.9 494.1
67296
2025-313BA 2026-01-08 97.41 94.64 507.5 495.1
67297
2025-313BB 2026-01-08 97.41 94.64 507.1 495.1

The majority of payloads were in a near-circular 500 kilometer orbit, but at least five objects were in the unexpected orbits. It appeared that the Fregat had failed to form its third target orbit and, as a result, the Marafon-IoT prototypes were released into a wrong orbit. Given the previous Iranian statement, it appears that the problems started during the release of the Paya spacecraft and, possibly, culminated with the failure of the Fregat to form its final target orbit, as well as preventing the space tug from performing its pre-programmed deorbiting burn.

On Jan. 21, 2026, OKB Fakel announced first tests of its electric propulsion system with the SPD-70 engine installed aboard Aist-2T No. 1 satellite. Indeed, the US tracking data did show that one of the satellites, believed to be a member of the Aist-T pair, had boosted its orbit:

NORAD ID
Object ID
Epoch
Inclination
Period
Apogee
Perigee
67253
2025-313F
2026-01-08T13:17:20.723712
97.1
91.95
378
363
67254
2025-313G
2026-01-08T13:17:52.151712
97.1
92.01
379
367

 

To be continued

 

insider content

The article by Anatoly Zak; Last update: January 21, 2026

Page editor: Alain Chabot; Last edit: December 27, 2025

All rights reserved

insider content

Aist-2T

The second and third stages of the Soyuz-2-1b rocket intended for the Aist-2T mission during processing in Vostochny. Click to enlarge. Credit: RKTs Progress


Aist-2T

Polytech-Universe-16 satellite developed at St. Petersburg Polytechnic University. Click to enlarge. Credit: RKTs Progress


Aist-2T

A close-up view of the two Aist-2T satellites after their integration with the Fregat upper stage. Click to enlarge. Credit: RKTs Progress


Aist-2T

A close-up view of launch containers for deployment of cubesats during the Aist-2T mission during integration of the payload section on Dec. 22, 2025. Click to enlarge. Credit: RKTs Progress


Aist-2T

The fully assembled payload section of the Aist-2T mission under its 81KS payload fairing on Dec. 22, 2025. Click to enlarge. Credit: Roskosmos


Aist-2T

A close-up view of an Iranian imaging satellite during integration for the Aist-2T mission. Click to enlarge. Credit: RKTs Progress


fregat

The four boosters of the first stage separate from the Soyuz-2-1b rocket as seen by an onboard camera during the Aist-2T launch on Dec. 28, 2025. Credit: Roskosmos


fregat

The Fregat upper stage separation during the Aist-2T mission as seen by a camera on the third stage of the Soyuz-2-1b launch vehicle. Credit: Roskosmos