DECAYED

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.

Not visible in the next 10 days
Identifier
61506, 2024-177D
Orbit
Decayed
Last TLE update
3 months 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)
2024-09-27 (7 months ago)
Launch vehicle
CHANG ZHENG 2D
Launch site
Jiuquan Satellite Launch Center, China (JSC)
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 3 months 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
Visualization observer readout
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 DEB Visibility forecast

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