JIELONG 3 DEB, 62575

Orbit data source: Space-Track

JIELONG 3 DEB, 62575 is space debris in LEO originally from a launch on Mon, 13 Jan 2025 UTC launched from the Yellow Sea Launch Area, China (YSLA). 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
62575, 2025-007A
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Changzheng H.
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
2025-01-13 (10 months ago)
Launch vehicle
Unknown
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.5 m
Radar Cross Section
2.062 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 JIELONG 3 DEB
1 62575U 25007A   25305.46796781  .00002279  00000-0  36138-3 0  9996
2 62575  54.9852  15.6083 0011240 203.5611 156.4875 14.75644489 43149
Epoch: 2025-11-01T11:13Z
TLE epoch observation values (Epoch: 2025-11-01T11:13:52.418Z)
Latitude
-0.00005°
Longitude
166.14224°
Altitude
651.412 km
Speed
7.529 km/s
True Right ascension
01h 02m 25s
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
01:15:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.964 km
Perigee altitude
635.18 km
Semi-major axis
7,021.209 km
Eccentricity
0.00112
Inclination
54.9852°
RAAN
15.6083°
Arg. of periapsis
203.5611°
True anomaly
156.53882°
Mean anomaly
156.4875°
Eccentric anomaly
156.51317°
Mean motion
3.68914 °/min
Orbital period
97.58 mins
BSTAR
0.00036138
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