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, 3.4 m
Radar Cross Section
16.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 COSMOS 2610
1 68758U 26083F 26291.66076058 .00002485 00000-0 17035-3 0 9999
2 68758 97.8238 71.3997 0010441 4.0387 356.0922 15.06962777 27793Epoch: 2026-10-18T15:51Z
TLE epoch observation values (Epoch: 2026-10-18T15:51:29.714Z)
Latitude
-0.00002°
Longitude
166.37602°
Altitude
541.334 km
Speed
7.596 km/s
True Right ascension
04h 45m 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
19:09:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.715 km
Perigee altitude
535.263 km
Semi-major axis
6,920.626 km
Eccentricity
0.00104
Inclination
97.8238°
RAAN
71.3997°
Arg. of periapsis
4.0387°
True anomaly
356.08404°
Mean anomaly
356.0922°
Eccentric anomaly
356.08812°
Mean motion
3.76986 °/min
Orbital period
95.49 mins
BSTAR
0.00017035
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-19 09:30:58.120Z | 169.419° S | 2026-10-19 09:33:58.120Z | 290.051° WNW | 82.663° | 2026-10-19 09:36:58.120Z | 345.542° N |
| 5 mins | 2026-10-19 22:42:58.120Z | 348.87° N | 2026-10-19 22:44:58.120Z | 287.042° WNW | 48.396° | 2026-10-19 22:47:58.120Z | 215.843° SW |
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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