CZ-2C R/B, 62078

Orbit data source: Space-Track

CZ-2C R/B, 62078 is space debris in SSO originally from a launch on Sun, 24 Nov 2024 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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
62078, 2024-218A
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
~3,800 kg wet, ~3,800 kg dry
Launch date (UTC)
2024-11-24 (1 year ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.7 m
Radar Cross Section
23.715 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 CZ-2C R/B
1 62078U 24218A   25337.48787794  .00009946  00000-0  43516-3 0  9994
2 62078  97.5428 347.2599 0046549 336.4608  23.4496 15.21268138 56676
Epoch: 2025-12-03T11:42Z
TLE epoch observation values (Epoch: 2025-12-03T11:42:32.654Z)
Latitude
-0.00004°
Longitude
99.06589°
Altitude
475.738 km
Speed
7.644 km/s
True Right ascension
23h 09m 02s
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
15:06:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
530.997 km
Perigee altitude
466.972 km
Semi-major axis
6,877.121 km
Eccentricity
0.00465
Inclination
97.5428°
RAAN
347.2599°
Arg. of periapsis
336.4608°
True anomaly
23.66301°
Mean anomaly
23.4496°
Eccentric anomaly
23.55619°
Mean motion
3.80569 °/min
Orbital period
94.6 mins
BSTAR
0.00043516
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Other satellites on launch #218 in the year 2024 (2024-11-24 UTC)

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