COSMOS 2610, 68758
Orbit data source: Space-Track
COSMOS 2610, 68758 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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68758 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, 14.5 m
Radar Cross Section
16.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 COSMOS 2610
1 68758U 26083F 26215.75837060 .00001543 00000-0 10824-3 0 9996
2 68758 97.8113 354.3552 0009128 250.0086 110.0158 15.06698745 16366Epoch: 2026-08-03T18:12Z
TLE epoch observation values (Epoch: 2026-08-03T18:12:03.219Z)
Latitude
-0.00005°
Longitude
129.00491°
Altitude
551.525 km
Speed
7.585 km/s
True Right ascension
23h 37m 25s
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
12:48:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.615 km
Perigee altitude
536.98 km
Semi-major axis
6,921.434 km
Eccentricity
0.00091
Inclination
97.8113°
RAAN
354.3552°
Arg. of periapsis
250.0086°
True anomaly
110.11404°
Mean anomaly
110.0158°
Eccentric anomaly
110.06493°
Mean motion
3.7692 °/min
Orbital period
95.51 mins
BSTAR
0.00010824
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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 2610 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-04 08:42:18.540Z | 112.684° SE | 2026-08-04 08:44:18.540Z | 61.324° ENE | 26.304° | 2026-08-04 08:47:18.540Z | 10.389° NNE |
| 4 mins | 2026-08-04 10:17:18.540Z | 240.176° WSW | 2026-08-04 10:18:18.540Z | 258.835° W | 17.388° | 2026-08-04 10:21:18.540Z | 309.641° NW |
| 5 mins | 2026-08-04 21:53:18.540Z | 38.141° NE | 2026-08-04 21:55:18.540Z | 110.306° ESE | 37.07° | 2026-08-04 21:58:18.540Z | 173.299° 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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