CZ-4C R/B, 68761

Orbit data source: Space-Track

CZ-4C R/B, 68761 is space debris in SSO originally from a launch on Fri, 17 Apr 2026 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
68761, 2026-084B
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)
2026-04-17 (1 month ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 8.0 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 CZ-4C R/B
1 68761U 26084B   26138.81200067  .00000578  00000-0  60956-4 0  9992
2 68761  98.2893 214.6826 0122020 301.5452  57.3893 14.88591588  4719
Epoch: 2026-05-18T19:29Z
TLE epoch observation values (Epoch: 2026-05-18T19:29:16.857Z)
Latitude
-0.00009°
Longitude
45.86748°
Altitude
560.189 km
Speed
7.606 km/s
True Right ascension
14h 18m 43s
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
09:29:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
684.522 km
Perigee altitude
514.242 km
Semi-major axis
6,977.519 km
Eccentricity
0.0122
Inclination
98.2893°
RAAN
214.6826°
Arg. of periapsis
301.5452°
True anomaly
58.57679°
Mean anomaly
57.3893°
Eccentric anomaly
57.98207°
Mean motion
3.72385 °/min
Orbital period
96.67 mins
BSTAR
0.000060956
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Other satellites on launch #84 in the year 2026 (2026-04-17 UTC)

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