COSMOS 2582, 62903
Orbit data source: Space-Track
COSMOS 2582, 62903 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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62903 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, 0.8 m
Radar Cross Section
3.727 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 COSMOS 2582
1 62903U 25026B 26089.70680463 .00001589 00000-0 14391-3 0 9998
2 62903 81.9969 154.5634 0009027 322.3373 37.7214 14.94803431 62484Epoch: 2026-03-30T16:57Z
TLE epoch observation values (Epoch: 2026-03-30T16:57:47.920Z)
Latitude
0.00004°
Longitude
72.01925°
Altitude
581.052 km
Speed
7.573 km/s
True Right ascension
10h 18m 15s
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
23:08:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.29 km
Perigee altitude
573.728 km
Semi-major axis
6,958.146 km
Eccentricity
0.0009
Inclination
81.9969°
RAAN
154.5634°
Arg. of periapsis
322.3373°
True anomaly
37.78474°
Mean anomaly
37.7214°
Eccentric anomaly
37.75307°
Mean motion
3.73941 °/min
Orbital period
96.27 mins
BSTAR
0.00014391
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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 2582 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 | 2026-04-01 04:25:48.861Z | 155.343° SSE | 2026-04-01 04:28:48.861Z | 101.143° ESE | 30.247° | 2026-04-01 04:32:48.861Z | 26.348° NE |
| 4 mins | 2026-04-01 06:04:48.861Z | 262.698° W | 2026-04-01 06:06:48.861Z | 296.332° NW | 15.59° | 2026-04-01 06:08:48.861Z | 325.955° NNW |
| 6 mins | 2026-04-01 16:07:48.861Z | 345.913° N | 2026-04-01 16:10:48.861Z | 233.075° WSW | 43.623° | 2026-04-01 16:13:48.861Z | 180.341° SSW |
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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