CZ-2D R/B, 61445 (Decayed)
Orbit data source: Space-Track
CZ-2D R/B, 61445 was space debris in LEO originally from a launch on Fri, 27 Sep 2024 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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61445 intel report (Beta)
CZ-2D R/B details
Identifier | |
Orbit | Decayed |
Last TLE update | 1 month ago |
Origin | |
Manufacturer | BWYIC |
Mission | Decayed spacecraft |
Bus & Motor | CZ-2 STAGE 2, Unknown motor |
Mass | 4,006 kg wet, 4,006 kg dry |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 1 month ago
0 CZ-2D R/B
1 61445U 24177B 24315.22634495 .07484936 79825-5 67146-3 0 9995
2 61445 41.3775 239.1072 0007529 234.7996 251.2891 16.37905997 6994
Epoch: 2024-11-10T05:25Z
Definitive object data (Epoch: 2024-11-10T05:25:56.203Z)
Latitude | 32.45712° |
Longitude | -118.12239° |
Altitude | 173.711 km |
Speed | 7.806 km/s |
True Right ascension | 00h 52m 55s |
True Declination | 32° 17' 16" |
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 | 178.633 km |
Perigee altitude | 168.768 km |
Semi-major axis | 6,551.838 km |
Eccentricity | 0.0007529 |
Inclination | 41.3775° |
RAAN | 239.1072° |
Arg. of periapsis | 234.7996° |
True anomaly | 251.20741° |
Mean anomaly | 251.2891° |
Eccentric anomaly | 251.24825° |
Mean motion | 4.09259 °/min |
BSTAR | 0.00067146 |
Orbital period | 87.96 mins |
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Other satellites on launch #177 in the year 2024 (2024-09-27 UTC)
SJ-19, 61444 (Decayed) |
CZ-2D R/B, 61445 (Decayed) |
SJ-19 DEB, 61505 (Decayed) |
SJ-19 DEB, 61506 |
CZ-2D R/B Visibility forecast
Observer location: undefined°, undefined
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