CZ-4C R/B, 47696

Orbit data source: Space-Track

CZ-4C R/B, 47696 is space debris in LEO originally from a launch on Wed, 24 Feb 2021 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
47696, 2021-014F
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2021-02-24 (5 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 2.5 m
Radar Cross Section
14.536 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 CZ-4C R/B
1 47696U 21014F   26170.86296289 -.00000110  00000-0 -12150-4 0  9993
2 47696  63.4538 354.8924 0297459   1.8936 358.3154 13.68592421265712
Epoch: 2026-06-19T20:42Z
TLE epoch observation values (Epoch: 2026-06-19T20:42:39.993Z)
Latitude
-0.00009°
Longitude
136.13988°
Altitude
786.894 km
Speed
7.571 km/s
True Right ascension
23h 39m 34s
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
21:26:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,223.008 km
Perigee altitude
783.865 km
Semi-major axis
7,381.573 km
Eccentricity
0.02975
Inclination
63.4538°
RAAN
354.8924°
Arg. of periapsis
1.8936°
True anomaly
358.21133°
Mean anomaly
358.3154°
Eccentric anomaly
358.26376°
Mean motion
3.42231 °/min
Orbital period
105.19 mins
BSTAR
-0.00001215
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