CZ-2C R/B, 61873

Orbit data source: Space-Track

CZ-2C R/B, 61873 is space debris in SSO originally from a launch on Sat, 09 Nov 2024 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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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CZ-2C R/B details

Identifier	61873, 2024-203E
Orbit	SSO
Last TLE update	23 hours ago
Origin	CASC (CN / PRC)
Manufacturer	BWYIC
Mission	Spacecraft
Bus & Motor	CZ-2 STAGE 2, Unknown motor
Mass	4,006 kg wet, 4,006 kg dry
Launch date (UTC)	2024-11-09 (1 month ago)
Launch vehicle	Unknown
Launch site	Jiuquan Satellite Launch Center, China (JSC)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 23 hours ago

0 CZ-2C R/B
1 61873U 24203E   24347.89176168  .00009077  00000-0  39376-3 0  9996
2 61873  97.3823  51.7134 0100776  25.8458 334.7761 15.18002439  5114

Epoch: 2024-12-12T21:24Z

Definitive object data (Epoch: 2024-12-12T21:24:08.209Z)

Latitude	0.00003°
Longitude	8.61361°
Altitude	452.268 km
Speed	7.676 km/s
True Right ascension	03h 26m 51s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude	-77.1758°
Longitude	155.08447°
Altitude	576.918 km
Speed	7.55 km/s
Apparent Right ascension	08h 23m 15s
Apparent Declination	-64° 36' 41"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	19:13:08
Azimuth	196.696° SSW
Elevation	-63.287°
Doppler factor	1

Orbital elements

Apogee altitude	578.25 km
Perigee altitude	439.441 km
Semi-major axis	6,886.982 km
Eccentricity	0.0100776
Inclination	97.3823°
RAAN	51.7134°
Arg. of periapsis	25.8458°
True anomaly	334.27831°
Mean anomaly	334.7761°
Eccentric anomaly	334.52777°
Mean motion	3.79752 °/min
BSTAR	0.00039376
Orbital period	94.8 mins