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 spacecraft
Bus & Motor
UNK, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 COSMOS 2612
1 68762U 26083H 26155.30526842 .00002801 00000-0 19133-3 0 9998
2 68762 97.8529 293.1496 0014560 93.9610 266.3281 15.06953251 7269Epoch: 2026-06-04T07:19Z
TLE epoch observation values (Epoch: 2026-06-04T07:19:35.191Z)
Latitude
-0.00008°
Longitude
-69.49846°
Altitude
549.236 km
Speed
7.587 km/s
True Right ascension
19h 32m 35s
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
05:01:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
552.596 km
Perigee altitude
532.443 km
Semi-major axis
6,920.656 km
Eccentricity
0.00146
Inclination
97.8529°
RAAN
293.1496°
Arg. of periapsis
93.961°
True anomaly
266.16162°
Mean anomaly
266.3281°
Eccentric anomaly
266.24486°
Mean motion
3.76983 °/min
Orbital period
95.49 mins
BSTAR
0.00019133
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-04 22:13:21.849Z | 7.411° NNE | 2026-06-04 22:17:21.849Z | 244.126° WSW | 42.149° | 2026-06-04 22:20:21.849Z | 201.88° SSW |
| 5 mins | 2026-06-05 08:58:21.849Z | 143.058° SSE | 2026-06-05 09:00:21.849Z | 71.54° E | 39.832° | 2026-06-05 09:03:21.849Z | 358.835° 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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