COSMOS 2616, 68827
Orbit data source: Space-Track
COSMOS 2616, 68827 is a payload satellite owned by MO RF (CIS) in SSO that was launched on Thu, 23 Apr 2026 UTC via an ANGARA-1.2 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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68827 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
VNIIEMI?
Mission
Operational Defense Imaging
Bus & Motor
OO-MKA, Unknown motor
Mass
520 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
3.727 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 COSMOS 2616
1 68827U 26090B 26206.49491220 .00037832 00000-0 16433-3 0 9998
2 68827 96.6414 123.0855 0011277 248.2159 111.7914 15.84651155 14736Epoch: 2026-07-25T11:52Z
TLE epoch observation values (Epoch: 2026-07-25T11:52:40.414Z)
Latitude
0.00006°
Longitude
1.71072°
Altitude
323.317 km
Speed
7.713 km/s
True Right ascension
08h 12m 20s
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
18:19:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
321.702 km
Perigee altitude
306.609 km
Semi-major axis
6,692.292 km
Eccentricity
0.00113
Inclination
96.6414°
RAAN
123.0855°
Arg. of periapsis
248.2159°
True anomaly
111.91133°
Mean anomaly
111.7914°
Eccentric anomaly
111.85137°
Mean motion
3.96443 °/min
Orbital period
90.81 mins
BSTAR
0.00016433
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Other satellites on launch #90 in the year 2026 (2026-04-23 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 2616 Visibility
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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. |
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| COSMOS 2616 is likely not visible in the next few days. |
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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