COSMOS 2584(GLONASS), 63130
Orbit data source: Space-Track
COSMOS 2584(GLONASS), 63130 is a Commonwealth of Independent States-origin payload satellite in MEO that was launched on Sun, 02 Mar 2025 UTC via a SOYUZ-2-1B 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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63130 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Resehetnev ISS
Mission
Operational Defense Navigation
Bus & Motor
KAUR-4N, AOCS
Mass
974 kg wet, ~800 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
3.585 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 COSMOS 2584(GLONASS)
1 63130U 25042A 26275.60017059 .00000035 00000-0 00000-0 0 9994
2 63130 65.1526 69.1546 0006783 203.8155 156.1648 2.13103208 12339Epoch: 2026-10-02T14:24Z
TLE epoch observation values (Epoch: 2026-10-02T14:24:14.738Z)
Latitude
0.00006°
Longitude
-158.24026°
Altitude
19,146.178 km
Speed
3.951 km/s
True Right ascension
04h 36m 33s
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
07:42:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,146.702 km
Perigee altitude
19,112.099 km
Semi-major axis
25,507.538 km
Eccentricity
0.00068
Inclination
65.1526°
RAAN
69.1546°
Arg. of periapsis
203.8155°
True anomaly
156.19619°
Mean anomaly
156.1648°
Eccentric anomaly
156.1805°
Mean motion
0.53277 °/min
Orbital period
675.71 mins
BSTAR
0
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Other satellites on launch #42 in the year 2025 (2025-03-02 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 2584(GLONASS) 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. |
|---|---|---|---|---|---|---|---|
| 126 mins | 2026-10-04 13:50:00.948Z | 15.474° NNE | 2026-10-04 13:50:00.948Z | 15.474° NNE | 59.55° | 2026-10-04 15:56:00.948Z | 66.396° ENE |
| 83 mins | 2026-10-05 01:46:00.948Z | 335.118° NNW | 2026-10-05 02:27:00.948Z | 315.848° NNW | 14.808° | 2026-10-05 03:09:00.948Z | 295.203° NW |
| 280 mins | 2026-10-05 09:08:00.948Z | 168.885° S | 2026-10-05 11:20:00.948Z | 95.009° ESE | 77.89° | 2026-10-05 13:48:00.948Z | 43.972° NE |
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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