JIELONG-3 DEB, 68688

Orbit data source: Space-Track

JIELONG-3 DEB, 68688 is space debris in LEO originally from a launch on Sat, 11 Apr 2026 UTC launched from the South China Sea Launch Area (SCSLA). 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
68688, 2026-078B
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Changzheng H.
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-04-11 (1 month ago)
Launch vehicle
Unknown
Launch site
South China Sea Launch Area (SCSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 JIELONG-3 DEB
1 68688U 26078B   26140.58875770  .00000316  00000-0  98891-4 0  9998
2 68688  86.5871 290.7654 0249794 259.3029  97.9947 14.21593676  5544
Epoch: 2026-05-20T14:07Z
TLE epoch observation values (Epoch: 2026-05-20T14:07:48.665Z)
Latitude
0.00002°
Longitude
-159.43352°
Altitude
852.398 km
Speed
7.411 km/s
True Right ascension
19h 23m 03s
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
08:06:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
996.673 km
Perigee altitude
637.215 km
Semi-major axis
7,195.081 km
Eccentricity
0.02498
Inclination
86.5871°
RAAN
290.7654°
Arg. of periapsis
259.3029°
True anomaly
100.81591°
Mean anomaly
97.9947°
Eccentric anomaly
99.40667°
Mean motion
3.55623 °/min
Orbital period
101.23 mins
BSTAR
0.000098891
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Other satellites on launch #78 in the year 2026 (2026-04-11 UTC)

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