CZ-2D DEB, 44601 (Decayed)
Orbit data source: Space-Track
CZ-2D DEB, 44601 was space debris in SSO originally from a launch on Wed, 07 Oct 2015 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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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44601 intel report (Beta)
CZ-2D DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 7 months ago |
Origin | |
Manufacturer | Unknown |
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 7 months ago
0 CZ-2D DEB
1 44601U 15057E 24150.42155774 .06404224 28558-5 42626-2 0 9997
2 44601 98.0938 323.2239 0020702 302.3455 57.5826 16.16447861465733
Epoch: 2024-05-29T10:07Z
Definitive object data (Epoch: 2024-05-29T10:07:02.588Z)
Latitude | 0.00003° |
Longitude | -75.96648° |
Altitude | 225.098 km |
Speed | 7.776 km/s |
True Right ascension | 21h 32m 53s |
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 | 239.757 km |
Perigee altitude | 212.412 km |
Semi-major axis | 6,604.222 km |
Eccentricity | 0.0020702 |
Inclination | 98.0938° |
RAAN | 323.2239° |
Arg. of periapsis | 302.3455° |
True anomaly | 57.78314° |
Mean anomaly | 57.5826° |
Eccentric anomaly | 57.68284° |
Mean motion | 4.044 °/min |
BSTAR | 0.0042626 |
Orbital period | 89.02 mins |
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Other satellites on launch #57 in the year 2015 (2015-10-07 UTC)
LQSAT, 40958 |
LINGQIAO VIDEO A, 40959 |
LINGQIAO VIDEO B, 40960 |
JILIN 1, 40961 |
CZ-2D DEB, 44601 (Decayed) |
CZ-2D DEB Visibility forecast
Observer location: undefined°, undefined
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