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, 0.6 m
Radar Cross Section
16.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 3 hours ago
TLE from 3 hours ago
0 COSMOS 2612
1 68762U 26083H 26215.79108532 .00002366 00000-0 16142-3 0 9993
2 68762 97.8606 354.8669 0011495 245.9473 114.0552 15.07200058 16375Epoch: 2026-08-03T18:59Z
TLE epoch observation values (Epoch: 2026-08-03T18:59:09.771Z)
Latitude
0.00003°
Longitude
117.70706°
Altitude
551.072 km
Speed
7.585 km/s
True Right ascension
23h 39m 28s
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
11:46:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.718 km
Perigee altitude
533.809 km
Semi-major axis
6,919.9 km
Eccentricity
0.00115
Inclination
97.8606°
RAAN
354.8669°
Arg. of periapsis
245.9473°
True anomaly
114.17541°
Mean anomaly
114.0552°
Eccentric anomaly
114.11531°
Mean motion
3.77045 °/min
Orbital period
95.48 mins
BSTAR
0.00016142
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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 | 2026-08-03 22:44:24.407Z | 348.745° N | 2026-08-03 22:47:24.407Z | 275.025° WNW | 30.622° | 2026-08-03 22:50:24.407Z | 221.921° SW |
| 6 mins | 2026-08-04 09:27:24.407Z | 173.589° S | 2026-08-04 09:30:24.407Z | 290.69° WNW | 43.745° | 2026-08-04 09:33:24.407Z | 343.027° N |
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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