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 (2 years ago)
Launch vehicle
Unknown
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.9 m
Radar Cross Section
2.062 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 JIELONG 3 DEB
1 62575U 25007A   26315.60053526  .00001648  00000-0  26202-3 0  9997
2 62575  54.9835 281.5183 0012490  11.6110 348.5176 14.76955767 98553
Epoch: 2026-11-11T14:24Z
TLE epoch observation values (Epoch: 2026-11-11T14:24:46.246Z)
Latitude
-0.00002°
Longitude
14.57954°
Altitude
631.43 km
Speed
7.548 km/s
True Right ascension
18h 46m 04s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
19:48:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
647.68 km
Perigee altitude
630.151 km
Semi-major axis
7,017.053 km
Eccentricity
0.00125
Inclination
54.9835°
RAAN
281.5183°
Arg. of periapsis
11.611°
True anomaly
348.48906°
Mean anomaly
348.5176°
Eccentric anomaly
348.50334°
Mean motion
3.69242 °/min
Orbital period
97.5 mins
BSTAR
0.00026202
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