JIELONG 3 R/B, 58507

Orbit data source: Space-Track

JIELONG 3 R/B, 58507 is space debris in LEO originally from a launch on Tue, 05 Dec 2023 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
58507, 2023-190C
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)
2023-12-05 (3 years ago)
Launch vehicle
Unknown
Launch site
South China Sea Launch Area (SCSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.7 m
Radar Cross Section
2.651 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 JIELONG 3 R/B
1 58507U 23190C   26162.67671438  .00013405  00000-0  26392-3 0  9997
2 58507  86.5605 252.7568 0235163 280.3003  77.1806 15.22399635137586
Epoch: 2026-06-11T16:14Z
TLE epoch observation values (Epoch: 2026-06-11T16:14:28.122Z)
Latitude
-0.00005°
Longitude
109.12253°
Altitude
469.539 km
Speed
7.649 km/s
True Right ascension
16h 51m 01s
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
13:00:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
657.081 km
Perigee altitude
333.799 km
Semi-major axis
6,873.577 km
Eccentricity
0.02352
Inclination
86.5605°
RAAN
252.7568°
Arg. of periapsis
280.3003°
True anomaly
79.82451°
Mean anomaly
77.1806°
Eccentric anomaly
78.50094°
Mean motion
3.80863 °/min
Orbital period
94.52 mins
BSTAR
0.00026392
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Other satellites on launch #190 in the year 2023 (2023-12-05 UTC)

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