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 (2 months ago)
Launch vehicle
Unknown
Launch site
South China Sea Launch Area (SCSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.7 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

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

TLE from 14 hours ago
0 JIELONG-3 DEB
1 68688U 26078B   26166.56210829  .00000714  00000-0  22816-3 0  9997
2 68688  86.5893 280.6790 0252067 175.6468 184.7003 14.21629374  9234
Epoch: 2026-06-15T13:29Z
TLE epoch observation values (Epoch: 2026-06-15T13:29:26.156Z)
Latitude
0.00005°
Longitude
174.4733°
Altitude
1,003.781 km
Speed
7.257 km/s
True Right ascension
18h 42m 42s
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
13:40:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
998.185 km
Perigee altitude
635.462 km
Semi-major axis
7,194.96 km
Eccentricity
0.02521
Inclination
86.5893°
RAAN
280.679°
Arg. of periapsis
175.6468°
True anomaly
184.47082°
Mean anomaly
184.7003°
Eccentric anomaly
184.58485°
Mean motion
3.55632 °/min
Orbital period
101.23 mins
BSTAR
0.00022816
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Other satellites on launch #78 in the year 2026 (2026-04-11 UTC)

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