CZ-3B R/B, 59707 (Decayed)
Orbit data source: Space-Track
CZ-3B R/B, 59707 was space debris in LEO originally from a launch on Thu, 09 May 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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59707 intel report (Beta)
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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 month ago
TLE from 1 month ago
0 CZ-3B R/B
1 59707U 24087C 26181.63293675 .21002615 10192-4 29914-3 0 9990
2 59707 52.9130 236.7736 0133378 207.5522 151.8405 16.25762579 56221Epoch: 2026-06-30T15:11Z
TLE epoch observation values (Epoch: 2026-06-30T15:11:25.735Z)
Latitude
0.00001°
Longitude
90.21514°
Altitude
282.515 km
Speed
7.694 km/s
True Right ascension
15h 47m 05s
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
19:07:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
292.055 km
Perigee altitude
116.466 km
Semi-major axis
6,582.397 km
Eccentricity
0.01334
Inclination
52.913°
RAAN
236.7736°
Arg. of periapsis
207.5522°
True anomaly
152.55132°
Mean anomaly
151.8405°
Eccentric anomaly
152.19695°
Mean motion
4.06412 °/min
Orbital period
88.58 mins
BSTAR
0.00029914
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Other satellites on launch #87 in the year 2024 (2024-05-09 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-3B 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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