SOYUZ MS-26, 61043 (Decayed)
Orbit data source: Space-Track
SOYUZ MS-26, 61043 was a payload satellite owned by RKKE (CIS) in LEO that was launched on Wed, 11 Sep 2024 UTC via a SOYUZ-2-1A launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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61043 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
RKKE
Mission
Decayed Civil Spaceship
Bus & Motor
7K-S A48, SA
Mass
7,152 kg wet, 2,900 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + Cone + Sphere + 2 Pan, 5.3 m
Radar Cross Section
25.344 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 SOYUZ MS-26
1 61043U 24162A 25122.80241190 .00013988 00000-0 25885-3 0 9996
2 61043 51.6344 171.8584 0002186 73.9391 286.1838 15.49304274505759Epoch: 2025-05-02T19:15Z
TLE epoch observation values (Epoch: 2025-05-02T19:15:28.388Z)
Latitude
-0.00002°
Longitude
22.03631°
Altitude
419.087 km
Speed
7.661 km/s
True Right ascension
11h 27m 26s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:15:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
420.755 km
Perigee altitude
417.783 km
Semi-major axis
6,797.406 km
Eccentricity
0.00022
Inclination
51.6344°
RAAN
171.8584°
Arg. of periapsis
73.9391°
True anomaly
286.15974°
Mean anomaly
286.1838°
Eccentric anomaly
286.17177°
Mean motion
3.87283 °/min
Orbital period
92.96 mins
BSTAR
0.00025885
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Other satellites on launch #162 in the year 2024 (2024-09-11 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SOYUZ MS-26 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-08 21:36:29.912Z | 285.717° WNW | 2026-04-08 21:38:29.912Z | 218.362° SW | 32.915° | 2026-04-08 21:40:29.912Z | 158.117° S |
| 4 mins | 2026-04-09 14:11:29.912Z | 217.396° SW | 2026-04-09 14:12:29.912Z | 176.342° S | 42.871° | 2026-04-09 14:15:29.912Z | 56.813° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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