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: 10 hours ago
TLE from 10 hours ago
0 COSMOS 2515
1 41394U 16020A 25286.98575414 .00002444 00000-0 16769-3 0 9992
2 41394 97.9825 288.3124 0025530 57.1980 303.1700 15.06774919523324Epoch: 2025-10-13T23:39Z
TLE epoch observation values (Epoch: 2025-10-13T23:39:29.157Z)
Latitude
-0.00007°
Longitude
-89.33975°
Altitude
539.476 km
Speed
7.598 km/s
True Right ascension
19h 13m 14s
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
04:15:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
560.741 km
Perigee altitude
525.402 km
Semi-major axis
6,921.209 km
Eccentricity
0.00255
Inclination
97.9825°
RAAN
288.3124°
Arg. of periapsis
57.198°
True anomaly
302.92469°
Mean anomaly
303.17°
Eccentric anomaly
303.04739°
Mean motion
3.76938 °/min
Orbital period
95.51 mins
BSTAR
0.00016769
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-14 12:58:17.322Z | 18.442° NNE | 2025-10-14 13:01:17.322Z | 73.205° E | 42.983° | 2025-10-14 13:05:17.322Z | 186.578° SSW |
| 5 mins | 2025-10-14 23:43:17.322Z | 119.872° SE | 2025-10-14 23:45:17.322Z | 60.037° ENE | 29.664° | 2025-10-14 23:48:17.322Z | 6.423° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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