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 (1 month ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 CZ-2D R/B
1 68141U 26048C   26104.89892493  .00000800  00000-0  73293-4 0  9991
2 68141  35.1298 286.4200 0016457 279.1927  80.6920 14.95622224  4929
Epoch: 2026-04-14T21:34Z
TLE epoch observation values (Epoch: 2026-04-14T21:34:27.113Z)
Latitude
-0.00002°
Longitude
119.73844°
Altitude
577.542 km
Speed
7.575 km/s
True Right ascension
19h 05m 40s
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
20:49:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.09 km
Perigee altitude
572.176 km
Semi-major axis
6,961.77 km
Eccentricity
0.00165
Inclination
35.1298°
RAAN
286.42°
Arg. of periapsis
279.1927°
True anomaly
80.87816°
Mean anomaly
80.692°
Eccentric anomaly
80.78507°
Mean motion
3.73649 °/min
Orbital period
96.35 mins
BSTAR
0.000073293
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Other satellites on launch #48 in the year 2026 (2026-03-12 UTC)

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