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, 0.5 m
Radar Cross Section
2.062 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 JIELONG 3 DEB
1 62575U 25007A   26202.16316069  .00000852  00000-0  15079-3 0  9993
2 62575  54.9842  25.7028 0014953  96.4733 263.7970 14.76705774 81794
Epoch: 2026-07-21T03:54Z
TLE epoch observation values (Epoch: 2026-07-21T03:54:57.083Z)
Latitude
-0.00005°
Longitude
28.02812°
Altitude
641.959 km
Speed
7.537 km/s
True Right ascension
01h 42m 48s
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
03:23:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.201 km
Perigee altitude
629.214 km
Semi-major axis
7,017.845 km
Eccentricity
0.0015
Inclination
54.9842°
RAAN
25.7028°
Arg. of periapsis
96.4733°
True anomaly
263.62669°
Mean anomaly
263.797°
Eccentric anomaly
263.71184°
Mean motion
3.69179 °/min
Orbital period
97.51 mins
BSTAR
0.00015079
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