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 (2 months ago)
Launch vehicle
Unknown
Launch site
South China Sea Launch Area (SCSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.8 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 JIELONG-3 R/B
1 68690U 26078C   26166.61206649  .00012016  00000-0  54256-3 0  9992
2 68690  86.6438 279.3423 0441565 162.5044 199.1955 14.62607664  9508
Epoch: 2026-06-15T14:41Z
TLE epoch observation values (Epoch: 2026-06-15T14:41:22.544Z)
Latitude
-0.00006°
Longitude
155.10241°
Altitude
983.873 km
Speed
7.204 km/s
True Right ascension
18h 37m 22s
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
13:40:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
993.414 km
Perigee altitude
369.94 km
Semi-major axis
7,059.814 km
Eccentricity
0.04416
Inclination
86.6438°
RAAN
279.3423°
Arg. of periapsis
162.5044°
True anomaly
197.6146°
Mean anomaly
199.1955°
Eccentric anomaly
198.39704°
Mean motion
3.65892 °/min
Orbital period
98.39 mins
BSTAR
0.00054256
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Other satellites on launch #78 in the year 2026 (2026-04-11 UTC)

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