KZ-1A R/B, 62191 (Decayed)
Orbit data source: Space-Track
KZ-1A R/B, 62191 was space debris in LEO originally from a launch on Wed, 04 Dec 2024 UTC launched from the Xichang Space Center, China (XSC). 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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62191 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CASIC
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 0.7 m
Radar Cross Section
22.101 m²
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 KZ-1A R/B
1 62191U 24228B 24340.50398185 .33852827 12798-4 48036-3 0 9992
2 62191 46.0912 100.6897 0134994 6.8812 42.8048 16.25337093 138Epoch: 2024-12-05T12:05Z
TLE epoch observation values (Epoch: 2024-12-05T12:05:44.031Z)
Latitude
34.04097°
Longitude
-115.24715°
Altitude
142.054 km
Speed
7.864 km/s
True Right ascension
09h 23m 52s
True Declination
33° 51' 60"
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
22:00:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
295.477 km
Perigee altitude
117.697 km
Semi-major axis
6,584.724 km
Eccentricity
0.0135
Inclination
46.0912°
RAAN
100.6897°
Arg. of periapsis
6.8812°
True anomaly
43.86904°
Mean anomaly
42.8048°
Eccentric anomaly
43.3356°
Mean motion
4.06197 °/min
Orbital period
88.63 mins
BSTAR
0.00048036
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Other satellites on launch #228 in the year 2024 (2024-12-04 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.KZ-1A R/B 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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