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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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, 0.8 m
Radar Cross Section
3.727 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 COSMOS 2582
1 62903U 25026B 26033.74151652 .00001712 00000-0 15597-3 0 9991
2 62903 81.9944 211.6195 0010466 137.5219 222.6812 14.94588524 54122Epoch: 2026-02-02T17:47Z
TLE epoch observation values (Epoch: 2026-02-02T17:47:47.027Z)
Latitude
-0.00006°
Longitude
171.7411°
Altitude
592.049 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
17:04:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.96 km
Perigee altitude
573.393 km
Semi-major axis
6,958.813 km
Eccentricity
0.00105
Inclination
81.9944°
RAAN
211.6195°
Arg. of periapsis
137.5219°
True anomaly
222.59997°
Mean anomaly
222.6812°
Eccentric anomaly
222.64058°
Mean motion
3.73887 °/min
Orbital period
96.29 mins
BSTAR
0.00015597
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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 | 2026-02-03 23:16:39.905Z | 2.841° NNE | 2026-02-03 23:20:39.905Z | 101.839° ESE | 38.107° | 2026-02-03 23:23:39.905Z | 155.066° SSE |
| 6 mins | 2026-02-04 11:41:39.905Z | 147.087° SSE | 2026-02-04 11:44:39.905Z | 99.089° ESE | 24.38° | 2026-02-04 11:47:39.905Z | 40.228° NE |
| 4 mins | 2026-02-04 13:20:39.905Z | 257.817° W | 2026-02-04 13:21:39.905Z | 276.508° WNW | 19.63° | 2026-02-04 13:24:39.905Z | 329.901° 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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