CZ-2D R/B, 37932

Orbit data source: Space-Track

CZ-2D R/B, 37932 is space debris in SSO originally from a launch on Sun, 20 Nov 2011 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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Identifier
37932, 2011-068C
Orbit
SSO
Last TLE update
15 hours ago
Origin
Manufacturer
BWYIC
Mission
Spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
4,006 kg wet, 4,006 kg dry
Launch date (UTC)
2011-11-20 (14 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Sail, 4.0 m
Radar Cross Section
25.456 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 15 hours ago
0 CZ-2D R/B
1 37932U 11068C   25197.85690925  .00000080  00000-0  55135-4 0  9999
2 37932  98.8415 146.0787 0037266 143.8793 276.9038 14.22869681708796
Epoch: 2025-07-16T20:33Z
TLE epoch observation values (Epoch: 2025-07-16T20:33:56.959Z)
Latitude
59.28128°
Longitude
-112.43317°
Altitude
822.554 km
Speed
7.449 km/s
True Right ascension
08h 43m 56s
True Declination
59° 07' 53"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
44.25917°
Longitude
-105.37952°
Altitude
825.543 km
Speed
7.443 km/s
Apparent Right ascension
10h 44m 43s
Apparent Declination
5° 47' 30"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
00:22:40
Azimuth
32.061° NE
Elevation
-39.027°
Doppler factor
1
Orbital elements
Apogee altitude
839.623 km
Perigee altitude
786.027 km
Semi-major axis
7,190.962 km
Eccentricity
0.00373
Inclination
98.8415°
RAAN
146.0787°
Arg. of periapsis
143.8793°
True anomaly
Unknown
Mean anomaly
276.9038°
Eccentric anomaly
Unknown
Mean motion
3.55928 °/min
Orbital period
101.14 mins
BSTAR
0.000055135
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