CZ-3B R/B, 59916

Orbit data source: Space-Track

CZ-3B R/B, 59916 is space debris in HEO originally from a launch on Thu, 30 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
59916, 2024-104B
Orbit
HEO
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)
2024-05-30 (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 59916U 24104B   26171.19255934  .00057860  50722-6  19368-2 0  9993
2 59916  26.6396  60.3372 6594667  74.5878 345.1602  3.24252320 21521
Epoch: 2026-06-20T04:37Z
TLE epoch observation values (Epoch: 2026-06-20T04:37:17.126Z)
Latitude
-0.00005°
Longitude
82.6305°
Altitude
2,876.509 km
Speed
8.091 km/s
True Right ascension
04h 01m 27s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
21:33:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
25,625.537 km
Perigee altitude
189.224 km
Semi-major axis
19,285.518 km
Eccentricity
0.65947
Inclination
26.6396°
RAAN
60.3372°
Arg. of periapsis
74.5878°
True anomaly
285.1899°
Mean anomaly
345.1602°
Eccentric anomaly
321.78724°
Mean motion
0.81039 °/min
Orbital period
444.23 mins
BSTAR
0.0019368
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Other satellites on launch #104 in the year 2024 (2024-05-30 UTC)

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