JIELONG-3 R/B, 68690

Orbit data source: Space-Track

JIELONG-3 R/B, 68690 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
68690, 2026-078C
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Changzheng H.
Mission
Spacecraft
Bus & Motor
Unknown
Mass
500 kg wet, 500 kg dry
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: 5 hours ago

TLE from 5 hours ago
0 JIELONG-3 R/B
1 68690U 26078C   26138.82760043  .00003918  00000-0  18110-3 0  9997
2 68690  86.6415 290.7128 0440810 258.1486  96.9985 14.62016675  5448
Epoch: 2026-05-18T19:51Z
TLE epoch observation values (Epoch: 2026-05-18T19:51:44.677Z)
Latitude
-0.00001°
Longitude
116.26637°
Altitude
741.122 km
Speed
7.457 km/s
True Right ascension
19h 22m 51s
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
09:33:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
994.869 km
Perigee altitude
372.294 km
Semi-major axis
7,061.718 km
Eccentricity
0.04408
Inclination
86.6415°
RAAN
290.7128°
Arg. of periapsis
258.1486°
True anomaly
101.97248°
Mean anomaly
96.9985°
Eccentric anomaly
99.48959°
Mean motion
3.65744 °/min
Orbital period
98.43 mins
BSTAR
0.0001811
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Other satellites on launch #78 in the year 2026 (2026-04-11 UTC)

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