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: 19 hours ago
TLE from 19 hours ago
0 COSMOS 2582
1 62903U 25026B 26221.69765285 .00000646 00000-0 56781-4 0 9993
2 62903 81.9955 19.8836 0008905 234.8607 125.1779 14.95107440 82205Epoch: 2026-08-09T16:44Z
TLE epoch observation values (Epoch: 2026-08-09T16:44:37.206Z)
Latitude
-0.00001°
Longitude
170.53765°
Altitude
588.653 km
Speed
7.564 km/s
True Right ascension
01h 19m 32s
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
01:46:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.26 km
Perigee altitude
572.869 km
Semi-major axis
6,957.202 km
Eccentricity
0.00089
Inclination
81.9955°
RAAN
19.8836°
Arg. of periapsis
234.8607°
True anomaly
125.26125°
Mean anomaly
125.1779°
Eccentric anomaly
125.21958°
Mean motion
3.74017 °/min
Orbital period
96.25 mins
BSTAR
0.000056781
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-10 12:09:30.411Z | 232.545° WSW | 2026-08-10 12:12:30.411Z | 288.996° WNW | 24.463° | 2026-08-10 12:15:30.411Z | 340.33° N |
| 7 mins | 2026-08-10 22:13:30.411Z | 2.193° NNE | 2026-08-10 22:16:30.411Z | 70.512° E | 41.169° | 2026-08-10 22:20:30.411Z | 160.792° S |
| 6 mins | 2026-08-11 10:38:30.411Z | 142.047° SSE | 2026-08-11 10:40:30.411Z | 104.268° ESE | 26.261° | 2026-08-11 10:44:30.411Z | 30.92° NE |
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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