SZ-19 DEB, 63801 (Decayed)
Orbit data source: Space-Track
SZ-19 DEB, 63801 was space debris in LEO originally from a launch on Tue, 29 Oct 2024 UTC launched 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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63801 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Decayed Civil Spaceship
Bus & Motor
SHENZHOU OM, Unknown motor
Mass
~1,842 kg wet, ~1,500 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 2.1 m
Radar Cross Section
9.277 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 SZ-19 DEB
1 63801U 24194E 26071.58446799 .03800286 81201-5 37885-3 0 9994
2 63801 41.4522 140.9527 0003059 46.7637 313.3484 16.37093782 49696Epoch: 2026-03-12T14:01Z
TLE epoch observation values (Epoch: 2026-03-12T14:01:38.034Z)
Latitude
0.00001°
Longitude
120.31198°
Altitude
171.754 km
Speed
7.806 km/s
True Right ascension
09h 23m 48s
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
10:11:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
177.858 km
Perigee altitude
173.848 km
Semi-major axis
6,553.99 km
Eccentricity
0.00031
Inclination
41.4522°
RAAN
140.9527°
Arg. of periapsis
46.7637°
True anomaly
313.3229°
Mean anomaly
313.3484°
Eccentric anomaly
313.33565°
Mean motion
4.09058 °/min
Orbital period
88.01 mins
BSTAR
0.00037885
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Other satellites on launch #194 in the year 2024 (2024-10-29 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.SZ-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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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