COSMOS 2580, 62216
Orbit data source: Space-Track
COSMOS 2580, 62216 is a payload satellite owned by VVKO VKS (CIS) in LEO that was launched on Wed, 04 Dec 2024 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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62216 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
TSSKBP/ARSLO
Mission
Operational Defense Sigint
Bus & Motor
YANTAR'-LOTOS, 11D428
Mass
6,575 kg wet, ~6,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 3.1 m
Radar Cross Section
16.222 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 COSMOS 2580
1 62216U 24230A 26152.19479993 -.00000056 00000-0 13903-4 0 9997
2 62216 67.1477 89.7166 0006447 264.0503 95.9847 13.96671842 75909Epoch: 2026-06-01T04:40Z
TLE epoch observation values (Epoch: 2026-06-01T04:40:30.713Z)
Latitude
-0.00003°
Longitude
129.903°
Altitude
907.944 km
Speed
7.398 km/s
True Right ascension
05h 58m 51s
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
03:55:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
908.387 km
Perigee altitude
898.998 km
Semi-major axis
7,281.829 km
Eccentricity
0.00064
Inclination
67.1477°
RAAN
89.7166°
Arg. of periapsis
264.0503°
True anomaly
96.05817°
Mean anomaly
95.9847°
Eccentric anomaly
96.02143°
Mean motion
3.49287 °/min
Orbital period
103.07 mins
BSTAR
0.000013903
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Other satellites on launch #230 in the year 2024 (2024-12-04 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 2580 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-01 20:15:11.614Z | 156.101° SSE | 2026-06-01 20:19:11.614Z | 113.174° SE | 21.819° | 2026-06-01 20:24:11.614Z | 55.652° ENE |
| 9 mins | 2026-06-01 22:01:11.614Z | 232.897° WSW | 2026-06-01 22:05:11.614Z | 302.773° NW | 38.704° | 2026-06-01 22:10:11.614Z | 17.406° NNE |
| 7 mins | 2026-06-02 05:17:11.614Z | 5.766° NNE | 2026-06-02 05:20:11.614Z | 43.804° NE | 22.454° | 2026-06-02 05:24:11.614Z | 93.594° ESE |
| 10 mins | 2026-06-02 07:02:11.614Z | 321.478° NNW | 2026-06-02 07:07:11.614Z | 226.595° WSW | 40.55° | 2026-06-02 07:12:11.614Z | 168.728° S |
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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