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 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: 10 hours ago
TLE from 10 hours ago
0 COSMOS 2610
1 68758U 26083F 26155.31910506 .00003132 00000-0 21630-3 0 9991
2 68758 97.8044 293.1110 0012082 97.6363 262.6236 15.06463312 7265Epoch: 2026-06-04T07:39Z
TLE epoch observation values (Epoch: 2026-06-04T07:39:30.677Z)
Latitude
-0.00003°
Longitude
-74.5319°
Altitude
551.162 km
Speed
7.586 km/s
True Right ascension
19h 32m 26s
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
03:44:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
552.382 km
Perigee altitude
535.655 km
Semi-major axis
6,922.156 km
Eccentricity
0.00121
Inclination
97.8044°
RAAN
293.111°
Arg. of periapsis
97.6363°
True anomaly
262.48632°
Mean anomaly
262.6236°
Eccentric anomaly
262.55496°
Mean motion
3.76861 °/min
Orbital period
95.53 mins
BSTAR
0.0002163
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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 | 2026-06-04 22:35:21.612Z | 336.153° NNW | 2026-06-04 22:37:21.612Z | 271.81° WNW | 31.037° | 2026-06-04 22:40:21.612Z | 220.297° SW |
| 6 mins | 2026-06-05 09:18:21.612Z | 173.718° S | 2026-06-05 09:20:21.612Z | 226.357° WSW | 44.215° | 2026-06-05 09:24:21.612Z | 344.936° 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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