COSMOS 2614, 68764
Orbit data source: Space-Track
COSMOS 2614, 68764 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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68764 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: 3 hours ago
TLE from 3 hours ago
0 COSMOS 2614
1 68764U 26083K 26215.77441654 .00001879 00000-0 13341-3 0 9994
2 68764 97.7848 353.4057 0005582 201.5354 158.5638 15.05964159 16360Epoch: 2026-08-03T18:35Z
TLE epoch observation values (Epoch: 2026-08-03T18:35:09.589Z)
Latitude
-0.00004°
Longitude
122.26305°
Altitude
555.208 km
Speed
7.582 km/s
True Right ascension
23h 33m 37s
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
11:49:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.414 km
Perigee altitude
541.684 km
Semi-major axis
6,923.686 km
Eccentricity
0.00056
Inclination
97.7848°
RAAN
353.4057°
Arg. of periapsis
201.5354°
True anomaly
158.58716°
Mean anomaly
158.5638°
Eccentric anomaly
158.57548°
Mean motion
3.76736 °/min
Orbital period
95.56 mins
BSTAR
0.00013341
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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 2614 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 | 2026-08-03 22:20:35.399Z | 2.475° NNE | 2026-08-03 22:23:35.399Z | 273.644° WNW | 41.364° | 2026-08-03 22:26:35.399Z | 206.549° SW |
| 6 mins | 2026-08-04 09:04:35.399Z | 152.323° SSE | 2026-08-04 09:07:35.399Z | 35.664° NE | 40.376° | 2026-08-04 09:10:35.399Z | 354.874° 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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