CZ-5 R/B, 41839 (Decayed)
Orbit data source: Space-Track
CZ-5 R/B, 41839 was space debris in LEO originally from a launch on Thu, 03 Nov 2016 UTC launched from the Wenchang Satellite Launch Center (WSC). 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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41839 intel report (Beta)
CZ-5 R/B details
Identifier | |
Orbit | Decayed |
Last TLE update | 6 months ago |
Origin | |
Manufacturer | CALT |
Mission | Decayed spacecraft |
Bus & Motor | CZ-5 H5-2, Unknown motor |
Mass | 5,100 kg wet, 5,100 kg dry |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Step Cyl, 10.6 m |
Radar Cross Section | 46.821 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 6 months ago
0 CZ-5 R/B
1 41839U 16065B 24194.02840997 .37109488 -18354-4 78870-3 0 9991
2 41839 19.1857 91.2608 0297245 43.9485 78.8439 15.85585105119706
Epoch: 2024-07-12T00:40Z
Definitive object data (Epoch: 2024-07-12T00:40:54.621Z)
Latitude | 15.46635° |
Longitude | -81.62584° |
Altitude | 278.663 km |
Speed | 7.764 km/s |
True Right ascension | 14h 36m 02s |
True Declination | 15° 22' 19" |
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 | 519.312 km |
Perigee altitude | 121.102 km |
Semi-major axis | 6,698.344 km |
Eccentricity | 0.0297245 |
Inclination | 19.1857° |
RAAN | 91.2608° |
Arg. of periapsis | 43.9485° |
True anomaly | 82.20797° |
Mean anomaly | 78.8439° |
Eccentric anomaly | 80.52375° |
Mean motion | 3.95906 °/min |
BSTAR | 0.0007887 |
Orbital period | 90.93 mins |
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Other satellites on launch #65 in the year 2016 (2016-11-03 UTC)
SJ-17, 41838 |
CZ-5 R/B, 41839 (Decayed) |
YZ-2 R/B, 41840 |
CZ-5 R/B Visibility forecast
Observer location: undefined°, undefined
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