SJ-19 DEB, 61506 (Decayed)
Orbit data source: Space-Track
SJ-19 DEB, 61506 was space debris in LEO originally from a launch on Fri, 27 Sep 2024 UTC via a CHANG ZHENG 2D launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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61506 intel report (Beta)
SJ-19 DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 1 month ago |
Origin | |
Manufacturer | CAST |
Mission | Decayed Civil Microgravity |
Bus & Motor | FSW-1, Unknown motor |
Mass | 3,550 kg wet, ~2,000 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Cyl, 2.2 m |
Radar Cross Section | 4.665 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 1 month ago
0 SJ-19 DEB
1 61506U 24177D 25009.31512986 .06246859 83581-5 24147-3 0 9991
2 61506 41.5818 219.4562 0005321 297.9087 235.7666 16.43965099 14315
Epoch: 2025-01-09T07:33Z
Definitive object data (Epoch: 2025-01-09T07:33:47.219Z)
Latitude | 4.19499° |
Longitude | 172.19966° |
Altitude | 156.384 km |
Speed | 7.814 km/s |
True Right ascension | 02h 18m 58s |
True Declination | 4° 10' 04" |
Sunlit | Object was in full shadow at TLE epoch |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
Apogee altitude | 161.045 km |
Perigee altitude | 154.09 km |
Semi-major axis | 6,535.705 km |
Eccentricity | 0.0005321 |
Inclination | 41.5818° |
RAAN | 219.4562° |
Arg. of periapsis | 297.9087° |
True anomaly | 235.71621° |
Mean anomaly | 235.7666° |
Eccentric anomaly | 235.7414° |
Mean motion | 4.10776 °/min |
BSTAR | 0.00024147 |
Orbital period | 87.64 mins |
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Other satellites on launch #177 in the year 2024 (2024-09-27 UTC)
SJ-19, 61444 (Decayed) |
CZ-2D R/B, 61445 (Decayed) |
SJ-19 DEB, 61505 (Decayed) |
SJ-19 DEB, 61506 (Decayed) |
SJ-19 DEB Visibility forecast
Observer location: undefined°, undefined
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