COSMOS 2609, 68754
Orbit data source: Space-Track
COSMOS 2609, 68754 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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68754 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, 0.6 m
Radar Cross Section
16.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 COSMOS 2609
1 68754U 26083B 26215.64901596 .00001926 00000-0 13803-3 0 9991
2 68754 98.1279 7.1568 0010498 223.8200 136.2193 15.05669554 16372Epoch: 2026-08-03T15:34Z
TLE epoch observation values (Epoch: 2026-08-03T15:34:34.978Z)
Latitude
-0.00006°
Longitude
-178.71803°
Altitude
557.756 km
Speed
7.58 km/s
True Right ascension
00h 28m 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
10:54:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
553.738 km
Perigee altitude
539.199 km
Semi-major axis
6,924.605 km
Eccentricity
0.00105
Inclination
98.1279°
RAAN
7.1568°
Arg. of periapsis
223.82°
True anomaly
136.30246°
Mean anomaly
136.2193°
Eccentric anomaly
136.26089°
Mean motion
3.76661 °/min
Orbital period
95.58 mins
BSTAR
0.00013803
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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 2609 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 22:31:48.806Z | 36.157° NE | 2026-08-03 22:34:48.806Z | 98.042° ESE | 29.233° | 2026-08-03 22:37:48.806Z | 160.282° S |
| 4 mins | 2026-08-04 10:51:48.806Z | 225.995° WSW | 2026-08-04 10:53:48.806Z | 276.773° WNW | 24.648° | 2026-08-04 10:55:48.806Z | 314.483° NW |
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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