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: 1 day ago
TLE from 1 day ago
0 COSMOS 2581
1 62902U 25026A 25308.48122155 .00001871 00000-0 17259-3 0 9994
2 62902 81.9935 303.6318 0012007 82.1003 278.1578 14.94133234 40651Epoch: 2025-11-04T11:32Z
TLE epoch observation values (Epoch: 2025-11-04T11:32:57.541Z)
Latitude
-0.00012°
Longitude
86.4244°
Altitude
586.925 km
Speed
7.567 km/s
True Right ascension
20h 14m 31s
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
08:31:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.448 km
Perigee altitude
573.734 km
Semi-major axis
6,960.228 km
Eccentricity
0.0012
Inclination
81.9935°
RAAN
303.6318°
Arg. of periapsis
82.1003°
True anomaly
278.02157°
Mean anomaly
278.1578°
Eccentric anomaly
278.08969°
Mean motion
3.73773 °/min
Orbital period
96.32 mins
BSTAR
0.00017259
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-06 00:38:17.196Z | 194.882° SSW | 2025-11-06 00:42:17.196Z | 327.367° NNW | 41.935° | 2025-11-06 00:45:17.196Z | 2.767° NNE |
| 5 mins | 2025-11-06 10:44:17.196Z | 33.878° NE | 2025-11-06 10:46:17.196Z | 72.088° E | 21.812° | 2025-11-06 10:49:17.196Z | 124.18° SE |
| 5 mins | 2025-11-06 12:21:17.196Z | 312.283° NW | 2025-11-06 12:23:17.196Z | 274.968° WNW | 22.256° | 2025-11-06 12:26:17.196Z | 221.168° SW |
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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