COSMOS 2459 (GLONASS), 36400
Orbit data source: Space-Track
COSMOS 2459 (GLONASS), 36400 is a Commonwealth of Independent States-origin payload satellite in MEO that was launched on Mon, 01 Mar 2010 UTC via a PROTON-M/DM-2 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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36400 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Resehetnev ISS
Mission
Non-operational Defense Navigation
Bus & Motor
URAGAN, Unknown motor
Mass
1,450 kg wet, ~1,200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 1 Ant + 2 Pan, 3.9 m
Radar Cross Section
8.467 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 COSMOS 2459 (GLONASS)
1 36400U 10007A 25305.42322968 -.00000003 00000-0 00000-0 0 9996
2 36400 65.5716 322.2792 0025568 342.2344 18.1992 2.13116779121977Epoch: 2025-11-01T10:09Z
TLE epoch observation values (Epoch: 2025-11-01T10:09:27.044Z)
Latitude
0.42896°
Longitude
129.16889°
Altitude
19,067.353 km
Speed
3.963 km/s
True Right ascension
21h 29m 56s
True Declination
0° 25' 42"
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
10:42:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,193.518 km
Perigee altitude
19,063.089 km
Semi-major axis
25,506.44 km
Eccentricity
0.00256
Inclination
65.5716°
RAAN
322.2792°
Arg. of periapsis
342.2344°
True anomaly
18.29099°
Mean anomaly
18.1992°
Eccentric anomaly
18.24506°
Mean motion
0.53281 °/min
Orbital period
675.67 mins
BSTAR
0
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Other satellites on launch #7 in the year 2010 (2010-03-01 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 2459 (GLONASS) 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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2025-11-02 14:54:38.305Z | 191.36° SSW | 2025-11-02 14:54:38.305Z | 191.36° SSW | 17.156° | 2025-11-02 15:09:38.305Z | 190.083° SSW |
| 79 mins | 2025-11-02 21:11:38.305Z | 62.135° ENE | 2025-11-02 21:50:38.305Z | 42.861° NE | 14.001° | 2025-11-02 22:30:38.305Z | 24.013° NE |
| 321 mins | 2025-11-03 08:19:38.305Z | 292.973° NW | 2025-11-03 11:19:38.305Z | 69.581° E | 44.51° | 2025-11-03 13:40:38.305Z | 168.878° S |
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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