SJ-19 DEB, 61505 (Decayed)
Orbit data source: Space-Track
SJ-19 DEB, 61505 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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61505 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Decayed spacecraft
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 Nozzle, 1.1 m
Radar Cross Section
3.283 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 SJ-19 DEB
1 61505U 24177C 24292.31661204 .04774915 42759-1 64047-2 0 9998
2 61505 41.5930 28.7319 0012063 32.1081 328.0510 16.09404383 1107Epoch: 2024-10-18T07:35Z
TLE epoch observation values (Epoch: 2024-10-18T07:35:55.28Z)
Latitude
-0°
Longitude
-112.53652°
Altitude
241.304 km
Speed
7.768 km/s
True Right ascension
01h 54m 55s
True Declination
0° 00' 00"
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
11:41:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
258.732 km
Perigee altitude
242.739 km
Semi-major axis
6,628.872 km
Eccentricity
0.00121
Inclination
41.593°
RAAN
28.7319°
Arg. of periapsis
32.1081°
True anomaly
327.97776°
Mean anomaly
328.051°
Eccentric anomaly
328.01439°
Mean motion
4.02146 °/min
Orbital period
89.52 mins
BSTAR
0.0064047
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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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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