CZ-2C R/B, 63127

Orbit data source: Space-Track

CZ-2C R/B, 63127 is space debris in SSO originally from a launch on Thu, 27 Feb 2025 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
63127, 2025-040C
Orbit
SSO
Last TLE update
7 hours ago
Origin
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
~3,800 kg wet, ~3,800 kg dry
Launch date (UTC)
2025-02-27 (6 months 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

TLE from 7 hours ago
0 CZ-2C R/B
1 63127U 25040C   25236.89232707  .00008418  00000-0  29564-3 0  9996
2 63127  97.1584 350.8791 0016827  51.8345 308.4409 15.29499114 27246
Epoch: 2025-08-24T21:24Z
TLE epoch observation values (Epoch: 2025-08-24T21:24:57.058Z)
Latitude
-0.00004°
Longitude
56.23514°
Altitude
473.257 km
Speed
7.633 km/s
True Right ascension
23h 23m 30s
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
19:35:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.782 km
Perigee altitude
462.721 km
Semi-major axis
6,852.388 km
Eccentricity
0.00168
Inclination
97.1584°
RAAN
350.8791°
Arg. of periapsis
51.8345°
True anomaly
308.28967°
Mean anomaly
308.4409°
Eccentric anomaly
308.36531°
Mean motion
3.82631 °/min
Orbital period
94.09 mins
BSTAR
0.00029564
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Other satellites on launch #40 in the year 2025 (2025-02-27 UTC)

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