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)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
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
Shape & HBR
Cyl, 1.1 m
Radar Cross Section
4.665 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 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 14315Epoch: 2025-01-09T07:33Z
TLE epoch observation values (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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:35:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
161.045 km
Perigee altitude
154.09 km
Semi-major axis
6,535.705 km
Eccentricity
0.00053
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
Orbital period
87.64 mins
BSTAR
0.00024147
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Other satellites on launch #177 in the year 2024 (2024-09-27 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SJ-19 DEB Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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