CZ-7A R/B, 60607 (Decayed)
Orbit data source: Space-Track
CZ-7A R/B, 60607 was space debris in HEO originally from a launch on Thu, 22 Aug 2024 UTC launched from the Wenchang Satellite Launch Center (WSC). 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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60607 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 CZ-7A R/B
1 60607U 24151B 24261.03072416 .01161033 20484-5 27794-2 0 9999
2 60607 14.6562 169.5289 6954656 190.0106 140.9887 2.77671165 530Epoch: 2024-09-17T00:44Z
TLE epoch observation values (Epoch: 2024-09-17T00:44:14.567Z)
Latitude
0.00022°
Longitude
162.05089°
Altitude
28,678.843 km
Speed
2.025 km/s
True Right ascension
11h 18m 15s
True Declination
0° 00' 01"
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
18:53:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
29,882.813 km
Perigee altitude
134.945 km
Semi-major axis
21,387.016 km
Eccentricity
0.69547
Inclination
14.6562°
RAAN
169.5289°
Arg. of periapsis
190.0106°
True anomaly
170.02557°
Mean anomaly
140.9887°
Eccentric anomaly
156.73057°
Mean motion
0.69393 °/min
Orbital period
518.78 mins
BSTAR
0.0027794
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Other satellites on launch #151 in the year 2024 (2024-08-22 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-7A 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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