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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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, 1.6 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 26272.76065845 .00001142 00000-0 10165-3 0 9990
2 62904 81.9970 327.7816 0011402 73.5195 286.7277 14.95210216 89826Epoch: 2026-09-29T18:15Z
TLE epoch observation values (Epoch: 2026-09-29T18:15:20.890Z)
Latitude
0.00001°
Longitude
45.42352°
Altitude
582.483 km
Speed
7.57 km/s
True Right ascension
21h 51m 07s
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
12:55:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.678 km
Perigee altitude
570.813 km
Semi-major axis
6,956.883 km
Eccentricity
0.00114
Inclination
81.997°
RAAN
327.7816°
Arg. of periapsis
73.5195°
True anomaly
286.60252°
Mean anomaly
286.7277°
Eccentric anomaly
286.66512°
Mean motion
3.74043 °/min
Orbital period
96.25 mins
BSTAR
0.00010165
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-01 04:06:29.040Z | 163.059° S | 2026-10-01 04:09:29.040Z | 102.631° ESE | 45.686° | 2026-10-01 04:13:29.040Z | 21.439° NNE |
| 6 mins | 2026-10-01 15:48:29.040Z | 337.162° NNW | 2026-10-01 15:51:29.040Z | 233.751° WSW | 53.669° | 2026-10-01 15:54:29.040Z | 188.167° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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