CZ-2D R/B, 44548

Orbit data source: Space-Track

CZ-2D R/B, 44548 is space debris in SSO originally from a launch on Wed, 25 Sep 2019 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
44548, 2019-063B
Orbit
SSO
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)
2019-09-25 (7 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
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 44548U 19063B   26171.34998080  .00000117  00000-0  49799-4 0  9993
2 44548  98.3506 127.2315 0007935 137.5095 222.6710 14.40829460354014
Epoch: 2026-06-20T08:23Z
TLE epoch observation values (Epoch: 2026-06-20T08:23:58.341Z)
Latitude
0.00005°
Longitude
92.67254°
Altitude
762.879 km
Speed
7.471 km/s
True Right ascension
08h 28m 55s
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
21:23:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
758.531 km
Perigee altitude
747.215 km
Semi-major axis
7,131.01 km
Eccentricity
0.00079
Inclination
98.3506°
RAAN
127.2315°
Arg. of periapsis
137.5095°
True anomaly
222.60941°
Mean anomaly
222.671°
Eccentric anomaly
222.6402°
Mean motion
3.60426 °/min
Orbital period
99.88 mins
BSTAR
0.000049799

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