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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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: 22 hours ago
TLE from 22 hours ago
0 COSMOS 2581
1 62902U 25026A 26123.77801183 .00000992 00000-0 88796-4 0 9995
2 62902 81.9931 119.8074 0009584 194.2486 165.8465 14.94885127 67582Epoch: 2026-05-03T18:40Z
TLE epoch observation values (Epoch: 2026-05-03T18:40:20.222Z)
Latitude
-0°
Longitude
-21.95354°
Altitude
592.238 km
Speed
7.56 km/s
True Right ascension
07h 59m 13s
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
00:40:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.424 km
Perigee altitude
573.087 km
Semi-major axis
6,957.892 km
Eccentricity
0.00096
Inclination
81.9931°
RAAN
119.8074°
Arg. of periapsis
194.2486°
True anomaly
165.87332°
Mean anomaly
165.8465°
Eccentric anomaly
165.85991°
Mean motion
3.73961 °/min
Orbital period
96.27 mins
BSTAR
0.000088796
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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 | 2026-05-04 23:43:10.521Z | 141.293° SSE | 2026-05-04 23:46:10.521Z | 85.045° E | 24.103° | 2026-05-04 23:49:10.521Z | 35.659° NE |
| 5 mins | 2026-05-05 01:21:10.521Z | 250.581° W | 2026-05-05 01:23:10.521Z | 288.457° WNW | 20.579° | 2026-05-05 01:26:10.521Z | 336.388° NNW |
| 6 mins | 2026-05-05 11:25:10.521Z | 357.88° N | 2026-05-05 11:27:10.521Z | 44.275° NE | 44.13° | 2026-05-05 11:31:10.521Z | 168.455° 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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