COSMOS 2615, 68826
Orbit data source: Space-Track
COSMOS 2615, 68826 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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68826 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: 16 hours ago
TLE from 16 hours ago
0 COSMOS 2615
1 68826U 26090A 26202.03830963 .00031006 00000-0 13154-3 0 9998
2 68826 96.6381 118.9675 0005802 274.9230 85.1380 15.85253497 14047Epoch: 2026-07-21T00:55Z
TLE epoch observation values (Epoch: 2026-07-21T00:55:09.952Z)
Latitude
0.00002°
Longitude
166.36229°
Altitude
318.484 km
Speed
7.717 km/s
True Right ascension
07h 55m 52s
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
06:11:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
316.34 km
Perigee altitude
308.577 km
Semi-major axis
6,690.595 km
Eccentricity
0.00058
Inclination
96.6381°
RAAN
118.9675°
Arg. of periapsis
274.923°
True anomaly
85.20425°
Mean anomaly
85.138°
Eccentric anomaly
85.17113°
Mean motion
3.96594 °/min
Orbital period
90.77 mins
BSTAR
0.00013154
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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 2615 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 2615 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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