CZ-2D R/B, 59396

Orbit data source: Space-Track

CZ-2D R/B, 59396 is space debris in LEO originally from a launch on Tue, 02 Apr 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
59396, 2024-063B
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
BWYIC
Mission
Spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
4,006 kg wet, 4,006 kg dry
Launch date (UTC)
2024-04-02 (2 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 4.5 m
Radar Cross Section
27.824 m², Large (>1 m²)

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

TLE from 2 days ago
0 CZ-2D R/B
1 59396U 24063B   26171.30679796  .00013909  00000-0  31592-3 0  9996
2 59396  34.7238  34.5138 0013224 138.0085 222.1646 15.42033858123875
Epoch: 2026-06-20T07:21Z
TLE epoch observation values (Epoch: 2026-06-20T07:21:47.343Z)
Latitude
-0.00005°
Longitude
15.54316°
Altitude
445.663 km
Speed
7.643 km/s
True Right ascension
02h 18m 03s
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
21:25:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
452.449 km
Perigee altitude
434.408 km
Semi-major axis
6,821.565 km
Eccentricity
0.00132
Inclination
34.7238°
RAAN
34.5138°
Arg. of periapsis
138.0085°
True anomaly
222.063°
Mean anomaly
222.1646°
Eccentric anomaly
222.11379°
Mean motion
3.85227 °/min
Orbital period
93.45 mins
BSTAR
0.00031592
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Other satellites on launch #63 in the year 2024 (2024-04-02 UTC)

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