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: 1 day ago
TLE from 1 day ago
0 COSMOS 2581
1 62902U 25026A 26109.72128351 .00000966 00000-0 86554-4 0 9994
2 62902 81.9939 134.1494 0008668 245.8436 114.1878 14.94851407 65482Epoch: 2026-04-19T17:18Z
TLE epoch observation values (Epoch: 2026-04-19T17:18:38.895Z)
Latitude
0.00001°
Longitude
26.66563°
Altitude
588.35 km
Speed
7.565 km/s
True Right ascension
08h 56m 35s
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
03:06:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.891 km
Perigee altitude
573.829 km
Semi-major axis
6,957.997 km
Eccentricity
0.00087
Inclination
81.9939°
RAAN
134.1494°
Arg. of periapsis
245.8436°
True anomaly
114.27837°
Mean anomaly
114.1878°
Eccentric anomaly
114.23309°
Mean motion
3.73953 °/min
Orbital period
96.27 mins
BSTAR
0.000086554
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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 | 2026-04-21 01:33:35.423Z | 147.059° SSE | 2026-04-21 01:36:35.423Z | 102.44° ESE | 23.403° | 2026-04-21 01:39:35.423Z | 42.879° NE |
| 4 mins | 2026-04-21 03:12:35.423Z | 254.763° W | 2026-04-21 03:14:35.423Z | 294.815° NW | 20.607° | 2026-04-21 03:16:35.423Z | 328.974° NNW |
| 7 mins | 2026-04-21 13:15:35.423Z | 356.513° N | 2026-04-21 13:18:35.423Z | 92.984° ESE | 44.303° | 2026-04-21 13:22:35.423Z | 168.254° 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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