CZ-6C R/B, 59681

Orbit data source: Space-Track

CZ-6C R/B, 59681 is space debris in SSO originally from a launch on Tue, 07 May 2024 UTC launched from the Taiyaun Space Center, China (TSC). 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
59681, 2024-085E
Orbit
SSO
Last TLE update
19 hours ago
Origin
Manufacturer
SAST
Mission
Operational spacecraft
Bus & Motor
CZ-6 STAGE 2, Unknown motor
Mass
3,000 kg wet, 3,000 kg dry
Launch date (UTC)
2024-05-07 (1 year ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history

TLE from 19 hours ago
0 CZ-6C R/B
1 59681U 24085E   25213.89561462  .00043351  00000-0  46444-3 0  9993
2 59681  97.3331 301.4638 0031253 146.2698 214.0558 15.63096255 69813
Epoch: 2025-08-01T21:29Z
TLE epoch observation values (Epoch: 2025-08-01T21:29:41.103Z)
Latitude
0.00002°
Longitude
28.30296°
Altitude
399.39 km
Speed
7.661 km/s
True Right ascension
20h 05m 51s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
58.57061°
Longitude
-138.79032°
Altitude
368.982 km
Speed
7.705 km/s
Apparent Right ascension
15h 08m 27s
Apparent Declination
27° 12' 16"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
06:12:21
Azimuth
40.557° NE
Elevation
-10.412°
Doppler factor
1
Orbital elements
Apogee altitude
396.732 km
Perigee altitude
354.517 km
Semi-major axis
6,753.762 km
Eccentricity
0.00313
Inclination
97.3331°
RAAN
301.4638°
Arg. of periapsis
146.2698°
True anomaly
213.85589°
Mean anomaly
214.0558°
Eccentric anomaly
213.95578°
Mean motion
3.91043 °/min
Orbital period
92.06 mins
BSTAR
0.00046444
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