JIELONG 3 R/B, 62586

Orbit data source: Space-Track

JIELONG 3 R/B, 62586 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.

Not visible in the next 10 days

JIELONG 3 R/B details

Identifier	62586, 2025-007M
Orbit	LEO
Last TLE update	16 hours ago
Origin	Changzheng H. (CN / PRC)
Manufacturer	Changzheng H.
Mission	Spacecraft
Bus & Motor	Unknown
Mass	500 kg wet, 500 kg dry
Launch date (UTC)	2025-01-13 (3 weeks ago)
Launch vehicle	Unknown
Launch site	Yellow Sea Launch Area, China (YSLA)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 16 hours ago

0 JIELONG 3 R/B
1 62586U 25007M   25035.48379173  .00644962  10396-4  10578-2 0  9995
2 62586  54.9364  24.8632 0239227  56.9784 305.3994 15.67141117  3470

Epoch: 2025-02-04T11:36Z

Definitive object data (Epoch: 2025-02-04T11:36:39.605Z)

Latitude	-0.00006°
Longitude	75.80971°
Altitude	277.337 km
Speed	7.794 km/s
True Right ascension	01h 39m 27s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-39.89109°
Longitude	-71.6925°
Altitude	535.702 km
Speed	7.505 km/s
Apparent Right ascension	16h 49m 33s
Apparent Declination	-40° 47' 28"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	05:54:52
Azimuth	99.303° ESE
Elevation	-77.543°
Doppler factor	1

Orbital elements

Apogee altitude	528.423 km
Perigee altitude	205.696 km
Semi-major axis	6,745.197 km
Eccentricity	0.0239227
Inclination	54.9364°
RAAN	24.8632°
Arg. of periapsis	56.9784°
True anomaly	303.12608°
Mean anomaly	305.3994°
Eccentric anomaly	304.26664°
Mean motion	3.91788 °/min
BSTAR	0.0010578
Orbital period	91.89 mins