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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Edit Public Description
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: 6 months ago
TLE from 6 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
21:31:39
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 | 2025-11-15 05:33:38.096Z | 337.602° N | 2025-11-15 05:35:38.096Z | 22.053° NNE | 19.506° | 2025-11-15 05:37:38.096Z | 67.583° E |
| 4 mins | 2025-11-15 07:10:38.096Z | 292.664° NW | 2025-11-15 07:12:38.096Z | 187.074° SSW | 39.15° | 2025-11-15 07:14:38.096Z | 143.489° SSE |
| 4 mins | 2025-11-15 23:48:38.096Z | 210.135° SW | 2025-11-15 23:50:38.096Z | 117.649° SE | 38.975° | 2025-11-15 23:52:38.096Z | 64.313° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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