JIELONG 3 R/B, 62586 (Decayed)
Orbit data source: Space-Track
JIELONG 3 R/B, 62586 was 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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62586 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
5 months ago
Origin
Manufacturer
Changzheng H.
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
500 kg wet, 500 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & history
TLE from 5 months ago
0 JIELONG 3 R/B
1 62586U 25007M 25058.03019657 .15427185 11914-4 26233-3 0 9994
2 62586 54.9157 275.1792 0032450 122.5767 38.4568 16.44195014 7058Epoch: 2025-02-27T00:43Z
TLE epoch observation values (Epoch: 2025-02-27T00:43:28.983Z)
Latitude
15.24986°
Longitude
-83.77821°
Altitude
138.516 km
Speed
7.836 km/s
True Right ascension
05h 36m 48s
True Declination
15° 09' 16"
Sunlit
Visualization orbit readout
No trajectory is available.
Visualization observer readout
No trajectory is available.
Orbital elements
Apogee altitude
175.84 km
Perigee altitude
133.442 km
Semi-major axis
6,532.778 km
Eccentricity
0.00325
Inclination
54.9157°
RAAN
275.1792°
Arg. of periapsis
122.5767°
True anomaly
38.6888°
Mean anomaly
38.4568°
Eccentric anomaly
38.57273°
Mean motion
4.11052 °/min
Orbital period
87.58 mins
BSTAR
0.00026233
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Other satellites on launch #7 in the year 2025 (2025-01-13 UTC)
JIELONG 3 R/B Visibility
Observer location: undefined°, undefined°
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Authenticating...
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