CZ-3B R/B, 59707

Orbit data source: Space-Track

CZ-3B R/B, 59707 is 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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Identifier
59707, 2024-087C
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2024-05-09 (2 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 CZ-3B R/B
1 59707U 24087C   26171.46210362  .04965545  79115-5  58736-3 0  9998
2 59707  52.9890 284.0828 0799122 169.6825 192.1702 14.57349908 54676
Epoch: 2026-06-20T11:05Z
TLE epoch observation values (Epoch: 2026-06-20T11:05:25.752Z)
Latitude
-0.00001°
Longitude
-150.95089°
Altitude
1,257.451 km
Speed
6.939 km/s
True Right ascension
18h 56m 19s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:28:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,267.813 km
Perigee altitude
136.231 km
Semi-major axis
7,080.159 km
Eccentricity
0.07991
Inclination
52.989°
RAAN
284.0828°
Arg. of periapsis
169.6825°
True anomaly
190.41223°
Mean anomaly
192.1702°
Eccentric anomaly
191.27499°
Mean motion
3.64316 °/min
Orbital period
98.82 mins
BSTAR
0.00058736
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Other satellites on launch #87 in the year 2024 (2024-05-09 UTC)

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