COSMOS 2612, 68762
Orbit data source: Space-Track
COSMOS 2612, 68762 is a payload satellite owned by VVKO VKS (CIS) in SSO that was launched on Thu, 16 Apr 2026 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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68762 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Unknown (RU)
Mission
Operational Imaging
Bus & Motor
UNK, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 3.4 m
Radar Cross Section
16.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 COSMOS 2612
1 68762U 26083H 26291.51771032 .00002106 00000-0 14210-3 0 9994
2 68762 97.8541 71.9986 0004460 258.9279 101.1447 15.07777458 27762Epoch: 2026-10-18T12:25Z
TLE epoch observation values (Epoch: 2026-10-18T12:25:30.171Z)
Latitude
-0.00001°
Longitude
-141.38599°
Altitude
546.652 km
Speed
7.588 km/s
True Right ascension
04h 47m 59s
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
17:46:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
543.08 km
Perigee altitude
536.909 km
Semi-major axis
6,918.132 km
Eccentricity
0.00045
Inclination
97.8541°
RAAN
71.9986°
Arg. of periapsis
258.9279°
True anomaly
101.19484°
Mean anomaly
101.1447°
Eccentric anomaly
101.16977°
Mean motion
3.7719 °/min
Orbital period
95.44 mins
BSTAR
0.0001421
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Other satellites on launch #83 in the year 2026 (2026-04-16 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 2612 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-19 09:15:39.606Z | 150.049° SSE | 2026-10-19 09:18:39.606Z | 77.555° E | 56.923° | 2026-10-19 09:21:39.606Z | 359.28° N |
| 6 mins | 2026-10-19 22:26:39.606Z | 10.53° NNE | 2026-10-19 22:29:39.606Z | 218.908° SW | 76.813° | 2026-10-19 22:32:39.606Z | 196.027° 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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