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.
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62586 intel report (Beta)
JIELONG 3 R/B details
Identifier | |
Orbit | LEO |
Last TLE update | 18 hours ago |
Origin | |
Manufacturer | Changzheng H. |
Mission | Spacecraft |
Bus & Motor | Unknown |
Mass | 500 kg wet, 500 kg dry |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 18 hours ago
0 JIELONG 3 R/B
1 62586U 25007M 25046.77725722 .01053340 10790-4 10956-2 0 9997
2 62586 54.9337 331.0168 0180403 88.3896 273.7806 15.85030639 5255
Epoch: 2025-02-15T18:39Z
Definitive object data (Epoch: 2025-02-15T18:39:15.023Z)
Latitude | -0.00009° |
Longitude | -94.81566° |
Altitude | 311.563 km |
Speed | 7.726 km/s |
True Right ascension | 22h 04m 04s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -15.20441° |
Longitude | -109.39661° |
Altitude | 352.207 km |
Speed | 7.677 km/s |
Apparent Right ascension | 23h 42m 30s |
Apparent Declination | -37° 04' 49" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 15:30:13 |
Azimuth | 105.317° ESE |
Elevation | -46.118° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 436.978 km |
Perigee altitude | 195.442 km |
Semi-major axis | 6,694.347 km |
Eccentricity | 0.0180403 |
Inclination | 54.9337° |
RAAN | 331.0168° |
Arg. of periapsis | 88.3896° |
True anomaly | 271.71521° |
Mean anomaly | 273.7806° |
Eccentric anomaly | 272.74816° |
Mean motion | 3.96261 °/min |
BSTAR | 0.0010956 |
Orbital period | 90.85 mins |
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Other satellites on launch #7 in the year 2025 (2025-01-13 UTC)
JIELONG 3 R/B Visibility forecast
Observer location: undefined°, undefined
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