CZ-3B R/B, 44077

Orbit data source: Space-Track

CZ-3B R/B, 44077 is space debris in HEO originally from a launch on Sun, 31 Mar 2019 UTC launched from the Xichang Space Center, China (XSC). 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
44077, 2019-017B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2019-03-31 (7 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

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

TLE from 2 days ago
0 CZ-3B R/B
1 44077U 19017B   26171.17275435  .00319653  57055-7  11793-2 0  9990
2 44077  26.7695 178.3670 5034321 109.1240 310.4138  5.75303038 90526
Epoch: 2026-06-20T04:08Z
TLE epoch observation values (Epoch: 2026-06-20T04:08:45.975Z)
Latitude
-0.00002°
Longitude
-152.21015°
Altitude
5,372.691 km
Speed
6.128 km/s
True Right ascension
11h 53m 29s
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
00:49:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
13,407.073 km
Perigee altitude
156.711 km
Semi-major axis
13,160.029 km
Eccentricity
0.50343
Inclination
26.7695°
RAAN
178.367°
Arg. of periapsis
109.124°
True anomaly
250.94266°
Mean anomaly
310.4138°
Eccentric anomaly
282.22316°
Mean motion
1.43767 °/min
Orbital period
250.41 mins
BSTAR
0.0011793
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Other satellites on launch #17 in the year 2019 (2019-03-31 UTC)

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