COSMOS 2583, 62904
Orbit data source: Space-Track
COSMOS 2583, 62904 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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62904 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, 14.5 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 2583
1 62904U 25026C 25308.34728647 .00002857 00000-0 26458-3 0 9995
2 62904 81.9942 303.7761 0012832 84.8058 275.4625 14.94137657 40611Epoch: 2025-11-04T08:20Z
TLE epoch observation values (Epoch: 2025-11-04T08:20:05.551Z)
Latitude
-0.00009°
Longitude
134.91735°
Altitude
587.249 km
Speed
7.567 km/s
True Right ascension
20h 15m 06s
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
11:07:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.009 km
Perigee altitude
573.146 km
Semi-major axis
6,960.214 km
Eccentricity
0.00128
Inclination
81.9942°
RAAN
303.7761°
Arg. of periapsis
84.8058°
True anomaly
275.3161°
Mean anomaly
275.4625°
Eccentric anomaly
275.3893°
Mean motion
3.73774 °/min
Orbital period
96.31 mins
BSTAR
0.00026458
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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 2583 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-06 00:37:43.005Z | 193.845° SSW | 2025-11-06 00:41:43.005Z | 265.359° W | 43.515° | 2025-11-06 00:45:43.005Z | 3.637° NNE |
| 5 mins | 2025-11-06 10:44:43.005Z | 40.548° NE | 2025-11-06 10:46:43.005Z | 82.204° E | 21.577° | 2025-11-06 10:49:43.005Z | 128.279° SE |
| 5 mins | 2025-11-06 12:21:43.005Z | 306.031° NW | 2025-11-06 12:23:43.005Z | 264.574° W | 22.242° | 2025-11-06 12:26:43.005Z | 216.977° 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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