CZ-4C R/B, 49010

Orbit data source: Space-Track

CZ-4C R/B, 49010 is space debris in SSO originally from a launch on Sun, 04 Jul 2021 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
49010, 2021-062C
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2021-07-04 (5 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 2.5 m
Radar Cross Section
14.536 m², Large (>1 m²)

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

TLE from 2 days ago
0 CZ-4C R/B
1 49010U 21062C   26171.24048720  .00000177  00000-0  46397-4 0  9997
2 49010  98.5278 260.3244 0130687 274.1163  84.5107 14.57224702263577
Epoch: 2026-06-20T05:46Z
TLE epoch observation values (Epoch: 2026-06-20T05:46:18.094Z)
Latitude
Longitude
-94.70894°
Altitude
697.468 km
Speed
7.511 km/s
True Right ascension
17h 21m 17s
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
21:36:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.741 km
Perigee altitude
606.757 km
Semi-major axis
7,077.386 km
Eccentricity
0.01307
Inclination
98.5278°
RAAN
260.3244°
Arg. of periapsis
274.1163°
True anomaly
86.00356°
Mean anomaly
84.5107°
Eccentric anomaly
85.25692°
Mean motion
3.6453 °/min
Orbital period
98.76 mins
BSTAR
0.000046397
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Other satellites on launch #62 in the year 2021 (2021-07-04 UTC)

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