COSMOS 2585, 63288
Orbit data source: Space-Track
COSMOS 2585, 63288 is a payload satellite owned by VVKO VKS (CIS) in LEO that was launched on Sun, 16 Mar 2025 UTC via an ANGARA-1.2 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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63288 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Resehetnev ISS
Mission
Operational Defense Communications
Bus & Motor
STRELA-3M, Unknown motor
Mass
280 kg wet, 280 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 1 Ant, 1.6 m
Radar Cross Section
1.583 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 COSMOS 2585
1 63288U 25054A 26077.90218715 .00000035 00000-0 18231-3 0 9994
2 63288 82.4936 134.8469 0023639 228.8117 131.0925 12.42895529 45645Epoch: 2026-03-18T21:39Z
TLE epoch observation values (Epoch: 2026-03-18T21:39:08.969Z)
Latitude
0.00003°
Longitude
-6.39976°
Altitude
1,509.311 km
Speed
7.105 km/s
True Right ascension
08h 59m 23s
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
08:11:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,510.308 km
Perigee altitude
1,473.101 km
Semi-major axis
7,869.841 km
Eccentricity
0.00236
Inclination
82.4936°
RAAN
134.8469°
Arg. of periapsis
228.8117°
True anomaly
131.29625°
Mean anomaly
131.0925°
Eccentric anomaly
131.19442°
Mean motion
3.10881 °/min
Orbital period
115.8 mins
BSTAR
0.00018231
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Other satellites on launch #54 in the year 2025 (2025-03-16 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 2585 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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2026-03-19 03:32:37.125Z | 150.802° SSE | 2026-03-19 03:39:37.125Z | 89.834° E | 33.798° | 2026-03-19 03:47:37.125Z | 21.526° NNE |
| 15 mins | 2026-03-19 05:29:37.125Z | 221.571° SW | 2026-03-19 05:36:37.125Z | 287.462° WNW | 33.879° | 2026-03-19 05:44:37.125Z | 354.942° N |
| 10 mins | 2026-03-19 13:44:37.125Z | 25.924° NE | 2026-03-19 13:49:37.125Z | 64.385° ENE | 18.485° | 2026-03-19 13:54:37.125Z | 102.347° ESE |
| 15 mins | 2026-03-19 15:40:37.125Z | 351.285° N | 2026-03-19 15:47:37.125Z | 235.422° WSW | 44.927° | 2026-03-19 15:55:37.125Z | 176.841° S |
| 7 mins | 2026-03-19 17:39:37.125Z | 308.119° NW | 2026-03-19 17:42:37.125Z | 285.853° WNW | 15.372° | 2026-03-19 17:46:37.125Z | 256.131° W |
| 10 mins | 2026-03-20 02:46:37.125Z | 116.253° SE | 2026-03-20 02:50:37.125Z | 84.305° E | 20.83° | 2026-03-20 02:56:37.125Z | 37.585° 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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