CZ-4C R/B, 53699

Orbit data source: Space-Track

CZ-4C R/B, 53699 is space debris in SSO originally from a launch on Fri, 02 Sep 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
53699, 2022-106B
Orbit
SSO
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)
2022-09-02 (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 53699U 22106B   26171.24622916  .00003767  00000-0  25028-3 0  9995
2 53699  98.0488 254.4783 0109373 140.7705 220.1511 15.03030208207385
Epoch: 2026-06-20T05:54Z
TLE epoch observation values (Epoch: 2026-06-20T05:54:34.199Z)
Latitude
-0.00001°
Longitude
-102.6278°
Altitude
618.943 km
Speed
7.518 km/s
True Right ascension
16h 57m 54s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
21:25:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.4 km
Perigee altitude
478.75 km
Semi-major axis
6,932.712 km
Eccentricity
0.01094
Inclination
98.0488°
RAAN
254.4783°
Arg. of periapsis
140.7705°
True anomaly
219.35134°
Mean anomaly
220.1511°
Eccentric anomaly
219.75039°
Mean motion
3.76 °/min
Orbital period
95.74 mins
BSTAR
0.00025028
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Other satellites on launch #106 in the year 2022 (2022-09-02 UTC)

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