FREGAT DEB, 45909 (Decayed)
Orbit data source: Space-Track
FREGAT DEB, 45909 was space debris in LEO originally from a launch on Mon, 18 Jul 2011 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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45909 intel report (Beta)
FREGAT DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 6 months ago |
Origin | |
Manufacturer | Lavochkin |
Mission | Decayed spacecraft |
Bus & Motor | Unknown |
Mass | Unknown |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 6 months ago
0 FREGAT DEB
1 45909U 11037EE 24177.66112808 .06291726 50178-1 28970-1 0 9994
2 45909 51.2844 343.0217 0046957 86.3952 274.2415 15.85688654175012
Epoch: 2024-06-25T15:52Z
Definitive object data (Epoch: 2024-06-25T15:52:01.466Z)
Latitude | -0.00005° |
Longitude | -169.26266° |
Altitude | 312.922 km |
Speed | 7.723 km/s |
True Right ascension | 22h 52m 05s |
True Declination | 0° 00' 00" |
Sunlit | Object was in full shadow at TLE epoch |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
Apogee altitude | 346.39 km |
Perigee altitude | 283.533 km |
Semi-major axis | 6,693.099 km |
Eccentricity | 0.0046957 |
Inclination | 51.2844° |
RAAN | 343.0217° |
Arg. of periapsis | 86.3952° |
True anomaly | 273.70466° |
Mean anomaly | 274.2415° |
Eccentric anomaly | 273.9731° |
Mean motion | 3.96371 °/min |
BSTAR | 0.02897 |
Orbital period | 90.82 mins |
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Other satellites on launch #37 in the year 2011 (2011-07-18 UTC)
FREGAT DEB Visibility forecast
Observer location: undefined°, undefined
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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