CZ-3C DEB, 42477

Orbit data source: Space-Track

CZ-3C DEB, 42477 is space debris in HEO originally from a launch on Fri, 24 Feb 2012 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.

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Last TLE update2 days ago
ManufacturerCALT
MissionSpacecraft
Bus & MotorUnknown
MassUnknown
Shape & HBRUnknown
Radar Cross SectionMedium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 2 days ago
0 CZ-3C DEB
1 42477U 12008AM  25090.40231256  .00014476  00000-0  29388-1 0  9997
2 42477  19.7705 229.7372 6943537 141.6783 297.5565  2.62884257 94134
Epoch: 2025-03-31T09:39Z
Definitive object data (Epoch: 2025-03-31T09:39:19.805Z)
Latitude0.00018°
Longitude-104.22836°
Altitude18,855.903 km
Speed3.69 km/s
True Right ascension15h 18m 29s
True Declination0° 00' 01"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude-19.64278°
Longitude156.34947°
Altitude10,827.923 km
Speed5.325 km/s
Apparent Right ascension09h 33m 23s
Apparent Declination-38° 05' 17"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time06:18:08
Azimuth143.679° SSE
Elevation0.098°
Doppler factor1
Orbital elements
Apogee altitude31,204.125 km
Perigee altitude401.368 km
Semi-major axis22,180.883 km
Eccentricity0.6943537
Inclination19.7705°
RAAN229.7372°
Arg. of periapsis141.6783°
True anomaly218.31485°
Mean anomaly297.5565°
Eccentric anomaly258.56294°
Mean motion0.65701 °/min
BSTAR0.029388
Orbital period547.93 mins
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CZ-3C DEB Visibility forecast

Observer location: undefined°, undefined°

Span
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Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
287 mins2025-04-02 03:25:08.666Z130.022° SE2025-04-02 07:06:08.666Z133.969° SE24.031°2025-04-02 08:12:08.666Z107.234° ESE
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