CZ-4C R/B, 54701

Orbit data source: Space-Track

CZ-4C R/B, 54701 is space debris in LEO originally from a launch on Mon, 12 Dec 2022 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
54701, 2022-169C
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)
2022-12-12 (4 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: 2 days ago

TLE from 2 days ago
0 CZ-4C R/B
1 54701U 22169C   26171.44641380  .00000168  00000-0  77584-4 0  9994
2 54701  59.9560  72.8992 0094619  69.8997 291.2199 14.51714097186598
Epoch: 2026-06-20T10:42Z
TLE epoch observation values (Epoch: 2026-06-20T10:42:50.152Z)
Latitude
-0.00009°
Longitude
3.52926°
Altitude
697.844 km
Speed
7.52 km/s
True Right ascension
04h 51m 35s
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
21:31:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
786.446 km
Perigee altitude
652.135 km
Semi-major axis
7,097.428 km
Eccentricity
0.00946
Inclination
59.956°
RAAN
72.8992°
Arg. of periapsis
69.8997°
True anomaly
290.20487°
Mean anomaly
291.2199°
Eccentric anomaly
290.71281°
Mean motion
3.62988 °/min
Orbital period
99.18 mins
BSTAR
0.000077584
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Other satellites on launch #169 in the year 2022 (2022-12-12 UTC)

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