KZ-1A R/B, 61199 (Decayed)
Orbit data source: Space-Track
KZ-1A R/B, 61199 was space debris in LEO originally from a launch on Fri, 20 Sep 2024 UTC via an FALCON 9 launch vehicle 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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61199 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
Launch site
Object type
Shape & HBR
Cyl, 0.7 m
Radar Cross Section
22.101 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 KZ-1A R/B
1 61199U 24170E 25110.16480910 .08808166 10333-4 66394-3 0 9990
2 61199 44.7016 10.9956 0041634 276.8081 202.5189 16.35127422 32409Epoch: 2025-04-20T03:57Z
TLE epoch observation values (Epoch: 2025-04-20T03:57:19.506Z)
Latitude
38.05043°
Longitude
-128.6812°
Altitude
206.22 km
Speed
7.773 km/s
True Right ascension
09h 16m 35s
True Declination
37° 52' 11"
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
18:19:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
207.839 km
Perigee altitude
153.226 km
Semi-major axis
6,558.669 km
Eccentricity
0.00416
Inclination
44.7016°
RAAN
10.9956°
Arg. of periapsis
276.8081°
True anomaly
202.33705°
Mean anomaly
202.5189°
Eccentric anomaly
202.42789°
Mean motion
4.0862 °/min
Orbital period
88.1 mins
BSTAR
0.00066394
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Other satellites on launch #170 in the year 2024 (2024-09-20 UTC)
KZ-1A R/B Visibility
Observer location: undefined°, undefined°
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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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Authenticating...
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