COSMOS 2581, 62902
Orbit data source: Space-Track
COSMOS 2581, 62902 is a payload satellite owned by MO RF (CIS) in LEO that was launched on Wed, 05 Feb 2025 UTC via a SOYUZ-2-1V launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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62902 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
VNIIEM
Mission
Operational Defense Imaging
Bus & Motor
EMKA, Unknown motor
Mass
~500 kg wet, 500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 1.3 m
Radar Cross Section
3.727 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 COSMOS 2581
1 62902U 25026A 25338.74958015 .00004718 00000-0 43660-3 0 9996
2 62902 81.9964 272.7780 0010070 350.1573 9.9447 14.94319569 45174Epoch: 2025-12-04T17:59Z
TLE epoch observation values (Epoch: 2025-12-04T17:59:23.724Z)
Latitude
-0.0001°
Longitude
-70.87242°
Altitude
580.616 km
Speed
7.574 km/s
True Right ascension
18h 11m 06s
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
09:35:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.52 km
Perigee altitude
574.504 km
Semi-major axis
6,959.649 km
Eccentricity
0.00101
Inclination
81.9964°
RAAN
272.778°
Arg. of periapsis
350.1573°
True anomaly
9.96465°
Mean anomaly
9.9447°
Eccentric anomaly
9.95467°
Mean motion
3.7382 °/min
Orbital period
96.3 mins
BSTAR
0.0004366
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Other satellites on launch #26 in the year 2025 (2025-02-05 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.COSMOS 2581 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-05 19:49:39.007Z | 146.525° SSE | 2025-12-05 19:52:39.007Z | 94.477° ESE | 25.111° | 2025-12-05 19:55:39.007Z | 37.651° NE |
| 4 mins | 2025-12-05 21:28:39.007Z | 261.185° W | 2025-12-05 21:29:39.007Z | 280.131° WNW | 19.191° | 2025-12-05 21:32:39.007Z | 331.278° NNW |
| 7 mins | 2025-12-06 07:31:39.007Z | 354.048° N | 2025-12-06 07:34:39.007Z | 136.668° SSE | 44.64° | 2025-12-06 07:38:39.007Z | 171.072° S |
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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