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: 1 day ago
TLE from 1 day ago
0 COSMOS 2582
1 62903U 25026B 25308.48193882 .00001689 00000-0 15569-3 0 9999
2 62903 81.9934 303.6316 0011984 82.1324 278.1255 14.94095162 40646Epoch: 2025-11-04T11:33Z
TLE epoch observation values (Epoch: 2025-11-04T11:33:59.514Z)
Latitude
-0.00001°
Longitude
86.16529°
Altitude
587.05 km
Speed
7.567 km/s
True Right ascension
20h 14m 31s
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
11:07:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.551 km
Perigee altitude
573.868 km
Semi-major axis
6,960.347 km
Eccentricity
0.0012
Inclination
81.9934°
RAAN
303.6316°
Arg. of periapsis
82.1324°
True anomaly
277.98952°
Mean anomaly
278.1255°
Eccentric anomaly
278.05751°
Mean motion
3.73763 °/min
Orbital period
96.32 mins
BSTAR
0.00015569
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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 | 2025-11-06 00:39:42.076Z | 196.726° SSW | 2025-11-06 00:42:42.076Z | 254.097° W | 42.83° | 2025-11-06 00:46:42.076Z | 2.761° NNE |
| 5 mins | 2025-11-06 10:45:42.076Z | 37.744° NE | 2025-11-06 10:47:42.076Z | 79.102° E | 22.264° | 2025-11-06 10:50:42.076Z | 127.791° SE |
| 5 mins | 2025-11-06 12:22:42.076Z | 307.603° NW | 2025-11-06 12:24:42.076Z | 268.012° W | 21.803° | 2025-11-06 12:27:42.076Z | 219.033° SW |
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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