FREGAT DEB, 45827 (Decayed)
Orbit data source: Space-Track
FREGAT DEB, 45827 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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45827 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 45827U 11037BM 24168.05010666 .10187582 31228+0 27244-1 0 9990
2 45827 51.3138 118.8033 0041951 246.4886 113.1709 16.00199680184332
Epoch: 2024-06-16T01:12Z
Definitive object data (Epoch: 2024-06-16T01:12:09.215Z)
Latitude | -0° |
Longitude | -164.04023° |
Altitude | 285.664 km |
Speed | 7.731 km/s |
True Right ascension | 07h 55m 12s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight 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 | 302.347 km |
Perigee altitude | 246.531 km |
Semi-major axis | 6,652.576 km |
Eccentricity | 0.0041951 |
Inclination | 51.3138° |
RAAN | 118.8033° |
Arg. of periapsis | 246.4886° |
True anomaly | 113.61193° |
Mean anomaly | 113.1709° |
Eccentric anomaly | 113.39151° |
Mean motion | 3.99999 °/min |
BSTAR | 0.027244 |
Orbital period | 90 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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