CZ-2D R/B, 68141

Orbit data source: Space-Track

CZ-2D R/B, 68141 is space debris in LEO originally from a launch on Thu, 12 Mar 2026 UTC launched from the Xichang Space Center, China (XSC). 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
68141, 2026-048C
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
BWYIC
Mission
Spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
4,006 kg wet, 4,006 kg dry
Launch date (UTC)
2026-03-12 (3 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 3.5 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 CZ-2D R/B
1 68141U 26048C   26171.24991307  .00000911  00000-0  82733-4 0  9990
2 68141  35.1285 247.0561 0015127 132.4763 227.7226 14.95783858 14868
Epoch: 2026-06-20T05:59Z
TLE epoch observation values (Epoch: 2026-06-20T05:59:52.489Z)
Latitude
-0.00001°
Longitude
-111.37986°
Altitude
585.962 km
Speed
7.566 km/s
True Right ascension
16h 28m 13s
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
07:20:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.662 km
Perigee altitude
572.602 km
Semi-major axis
6,961.269 km
Eccentricity
0.00151
Inclination
35.1285°
RAAN
247.0561°
Arg. of periapsis
132.4763°
True anomaly
227.59451°
Mean anomaly
227.7226°
Eccentric anomaly
227.65854°
Mean motion
3.73689 °/min
Orbital period
96.34 mins
BSTAR
0.000082733
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Other satellites on launch #48 in the year 2026 (2026-03-12 UTC)

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