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
Last TLE update
22 hours ago
Origin
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 (6 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

TLE from 22 hours ago
0 CZ-3B R/B
1 44077U 19017B   25199.50122902  .00059804 -20769-7  10155-2 0  9999
2 44077  26.8003 182.6206 5556272 221.0309  80.1440  4.83386539 73159
Epoch: 2025-07-18T12:01Z
TLE epoch observation values (Epoch: 2025-07-18T12:01:46.187Z)
Latitude
-0.00007°
Longitude
65.60214°
Altitude
11,204.367 km
Speed
4.286 km/s
True Right ascension
12h 10m 23s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
23.98043°
Longitude
126.29808°
Altitude
14,733.777 km
Speed
3.284 km/s
Apparent Right ascension
15h 19m 25s
Apparent Declination
12° 13' 31"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
22:54:30
Azimuth
294.901° NW
Elevation
-9.571°
Doppler factor
1
Orbital elements
Apogee altitude
16,612.476 km
Perigee altitude
189.248 km
Semi-major axis
14,778.999 km
Eccentricity
0.55563
Inclination
26.8003°
RAAN
182.6206°
Arg. of periapsis
221.0309°
True anomaly
138.99924°
Mean anomaly
80.144°
Eccentric anomaly
110.04974°
Mean motion
1.20802 °/min
Orbital period
298.01 mins
BSTAR
0.0010155
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