CZ-3C DEB, 44526

Orbit data source: Space-Track

CZ-3C DEB, 44526 is space debris in HEO originally from a launch on Sun, 31 Oct 2010 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 weeks 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 weeks ago
0 CZ-3C DEB
1 44526U 10057BL  25066.98803396  .00000618  00000-0  30178-2 0  9995
2 44526  21.7020 277.0751 7012445 347.6311   1.6015  2.49004335 84636
Epoch: 2025-03-07T23:42Z
Definitive object data (Epoch: 2025-03-07T23:42:46.134Z)
Latitude0.0008°
Longitude115.46679°
Altitude573.332 km
Speed9.866 km/s
True Right ascension18h 28m 23s
True Declination0° 00' 03"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude13.04305°
Longitude-106.60527°
Altitude20,333.535 km
Speed3.537 km/s
Apparent Right ascension04h 23m 30s
Apparent Declination4° 21' 10"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time22:21:51
Azimuth86.395° E
Elevation2.476°
Doppler factor1
Orbital elements
Apogee altitude32,745.895 km
Perigee altitude492.433 km
Semi-major axis22,997.301 km
Eccentricity0.7012445
Inclination21.702°
RAAN277.0751°
Arg. of periapsis347.6311°
True anomaly12.70552°
Mean anomaly1.6015°
Eccentric anomaly5.34241°
Mean motion0.62234 °/min
BSTAR0.0030178
Orbital period578.46 mins
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CZ-3C DEB Visibility forecast

Observer location: undefined°, undefined°

Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
123 mins2025-03-24 02:29:32.692Z268.885° W2025-03-24 03:17:32.692Z261.852° W14.039°2025-03-24 04:32:32.692Z259.925° W
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