COSMOS 2515, 41394
Orbit data source: Space-Track
COSMOS 2515, 41394 is a payload satellite owned by VVKO VKS (CIS) in SSO that was launched on Thu, 24 Mar 2016 UTC via a SOYUZ-2-1A 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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41394 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Arsenal
Mission
Operational Defense Imaging
Bus & Motor
BARS, AOCS
Mass
3,700 kg wet, ~3,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 5.0 m
Radar Cross Section
20.881 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 COSMOS 2515
1 41394U 16020A 25256.96709398 .00001450 00000-0 10198-3 0 9993
2 41394 97.9807 257.2098 0024822 152.7332 207.5203 15.06570509518806Epoch: 2025-09-13T23:12Z
TLE epoch observation values (Epoch: 2025-09-13T23:12:36.919Z)
Latitude
-0.00008°
Longitude
-84.13688°
Altitude
565 km
Speed
7.57 km/s
True Right ascension
17h 08m 50s
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
23:08:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
560.88 km
Perigee altitude
526.517 km
Semi-major axis
6,921.835 km
Eccentricity
0.00248
Inclination
97.9807°
RAAN
257.2098°
Arg. of periapsis
152.7332°
True anomaly
207.38923°
Mean anomaly
207.5203°
Eccentric anomaly
207.45473°
Mean motion
3.76887 °/min
Orbital period
95.52 mins
BSTAR
0.00010198
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Other satellites on launch #20 in the year 2016 (2016-03-24 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 2515 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 | 2025-09-14 12:31:57.484Z | 32.55° NE | 2025-09-14 12:34:57.484Z | 94.775° ESE | 31.294° | 2025-09-14 12:37:57.484Z | 163.431° S |
| 4 mins | 2025-09-14 23:16:57.484Z | 104.053° ESE | 2025-09-14 23:18:57.484Z | 63.393° ENE | 20.303° | 2025-09-14 23:20:57.484Z | 26.632° NE |
| 5 mins | 2025-09-15 00:50:57.484Z | 216.918° SW | 2025-09-15 00:52:57.484Z | 256.65° W | 23.393° | 2025-09-15 00:55:57.484Z | 315.785° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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