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: 20 hours ago
TLE from 20 hours ago
0 COSMOS 2581
1 62902U 25026A 26033.74146757 .00001998 00000-0 18238-3 0 9991
2 62902 81.9940 211.6203 0010955 136.9713 223.2365 14.94587161 54139Epoch: 2026-02-02T17:47Z
TLE epoch observation values (Epoch: 2026-02-02T17:47:42.798Z)
Latitude
-0.00002°
Longitude
171.75957°
Altitude
592.254 km
Speed
7.561 km/s
True Right ascension
14h 06m 28s
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
15:31:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.304 km
Perigee altitude
573.057 km
Semi-major axis
6,958.818 km
Eccentricity
0.0011
Inclination
81.994°
RAAN
211.6203°
Arg. of periapsis
136.9713°
True anomaly
223.15059°
Mean anomaly
223.2365°
Eccentric anomaly
223.19354°
Mean motion
3.73887 °/min
Orbital period
96.29 mins
BSTAR
0.00018238
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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 | 2026-02-03 23:17:00.993Z | 4.788° NNE | 2026-02-03 23:20:00.993Z | 67.137° ENE | 38.644° | 2026-02-03 23:24:00.993Z | 156.72° SSE |
| 6 mins | 2026-02-04 11:42:00.993Z | 143.363° SSE | 2026-02-04 11:45:00.993Z | 88.257° E | 24.558° | 2026-02-04 11:48:00.993Z | 36.216° NE |
| 5 mins | 2026-02-04 13:20:00.993Z | 249.04° W | 2026-02-04 13:22:00.993Z | 285.29° WNW | 19.993° | 2026-02-04 13:25:00.993Z | 334.526° NNW |
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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