DECAYED

CZ-2D R/B, 58142 (Decayed)

Orbit data source: Space-Track

CZ-2D R/B, 58142 was space debris in LEO originally from a launch on Mon, 23 Oct 2023 UTC launched from the Xichang Space Center, China (XSC). 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.

Not visible in the next 10 days
Identifier
58142, 2023-163B
Orbit
Decayed
Last TLE update
9 months 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)
2023-10-23 (2 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Sail, 4.5 m
Radar Cross Section
27.824 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 9 months ago
0 CZ-2D R/B
1 58142U 23163B   24282.52658632  .11432968  12836-5  23718-2 0  9992
2 58142  34.9547 199.7689 0004762 249.9087 287.0150 16.29904791 54135
Epoch: 2024-10-08T12:38Z
TLE epoch observation values (Epoch: 2024-10-08T12:38:17.058Z)
Latitude
1.7598°
Longitude
170.05464°
Altitude
190.522 km
Speed
7.795 km/s
True Right ascension
01h 09m 03s
True Declination
1° 44' 54"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
199.334 km
Perigee altitude
193.073 km
Semi-major axis
6,574.34 km
Eccentricity
0.00048
Inclination
34.9547°
RAAN
199.7689°
Arg. of periapsis
249.9087°
True anomaly
286.96281°
Mean anomaly
287.015°
Eccentric anomaly
286.98891°
Mean motion
4.0716 °/min
Orbital period
88.42 mins
BSTAR
0.0023718
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