DECAYED

CZ-4B R/B, 46481 (Decayed)

Orbit data source: Space-Track

CZ-4B R/B, 46481 was space debris in LEO originally from a launch on Sun, 27 Sep 2020 UTC launched from the Taiyaun Space Center, China (TSC). 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
46481, 2020-067D
Orbit
Decayed
Last TLE update
2 months ago
Origin
Manufacturer
SAST
Mission
Decayed spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2020-09-27 (5 years ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 4.932 m
Radar Cross Section
14.536 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 2 months ago
0 CZ-4B R/B
1 46481U 20067D   25063.05996941  .16327159  30540-5  27236-3 0  9991
2 46481  97.9670 267.0228 0007503 239.9305 279.4691 16.47815037246547
Epoch: 2025-03-04T01:26Z
Definitive object data (Epoch: 2025-03-04T01:26:21.357Z)
Latitude
20.48346°
Longitude
-93.6555°
Altitude
147.126 km
Speed
7.82 km/s
True Right ascension
06h 00m 00s
True Declination
20° 21' 38"
Sunlit
Object was in full shadow at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
146.812 km
Perigee altitude
137.028 km
Semi-major axis
6,520.057 km
Eccentricity
0.0007503
Inclination
97.967°
RAAN
267.0228°
Arg. of periapsis
239.9305°
True anomaly
279.38428°
Mean anomaly
279.4691°
Eccentric anomaly
279.42669°
Mean motion
4.12255 °/min
BSTAR
0.00027236
Orbital period
87.32 mins
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CZ-4B R/B Visibility forecast

Observer location: undefined°, undefined°

This satellite is decayed
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