CZ-3A R/B, 30324

Orbit data source: Space-Track

CZ-3A R/B, 30324 is space debris in HEO originally from a launch on Fri, 02 Feb 2007 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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Identifier
30324, 2007-003B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2007-02-02 (19 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.751 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 CZ-3A R/B
1 30324U 07003B   25293.83738329  .00003991  00000-0  10730-2 0  9991
2 30324  24.5627 188.0941 5772192 117.8332 311.4032  4.36391319222996
Epoch: 2025-10-20T20:05Z
TLE epoch observation values (Epoch: 2025-10-20T20:05:49.916Z)
Latitude
0.00001°
Longitude
-142.89119°
Altitude
8,062.639 km
Speed
5.478 km/s
True Right ascension
12h 32m 24s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
13:38:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,576.28 km
Perigee altitude
311.008 km
Semi-major axis
15,821.781 km
Eccentricity
0.57722
Inclination
24.5627°
RAAN
188.0941°
Arg. of periapsis
117.8332°
True anomaly
242.19054°
Mean anomaly
311.4032°
Eccentric anomaly
278.71261°
Mean motion
1.09059 °/min
Orbital period
330.1 mins
BSTAR
0.001073
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