CZ-4B R/B, 60250 (Decayed)
Orbit data source: Space-Track
CZ-4B R/B, 60250 was space debris in LEO originally from a launch on Fri, 19 Jul 2024 UTC launched from the Taiyaun Space Center, China (TSC). 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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60250 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Decayed spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT B
1 60250U 24130B 24235.98486666 .12432784 26111-5 26985-3 0 9992
2 60250 97.3929 308.5878 0019573 40.1387 46.3473 16.44862158 5536Epoch: 2024-08-22T23:38Z
TLE epoch observation values (Epoch: 2024-08-22T23:38:12.479Z)
Latitude
81.93115°
Longitude
-83.23061°
Altitude
157.598 km
Speed
7.824 km/s
True Right ascension
16h 12m 20s
True Declination
81° 52' 44"
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
15:54:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
162.478 km
Perigee altitude
136.924 km
Semi-major axis
6,527.838 km
Eccentricity
0.00196
Inclination
97.3929°
RAAN
308.5878°
Arg. of periapsis
40.1387°
True anomaly
46.50986°
Mean anomaly
46.3473°
Eccentric anomaly
46.42855°
Mean motion
4.11518 °/min
Orbital period
87.48 mins
BSTAR
0.00026985
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Other satellites on launch #130 in the year 2024 (2024-07-19 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.CZ-4B 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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