DECAYED

OBJECT B, 44487 (Decayed)

Orbit data source: Space-Track

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Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

OBJECT B, 44487 was a satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Sat, 17 Aug 2019 UTC via a JIELONG-1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.

Not visible in the next 10 days
Identifier
44487, 2019-052B
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
GUOG?
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 6U?, Unknown motor
Mass
8 kg wet, 8 kg dry
Launch date (UTC)
2019-08-17 (6 years ago)
Launch vehicle
JIELONG-1
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.105 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 6 months ago

TLE from 6 months ago
0 OBJECT B
1 44487U 19052B   25050.17604496  .05815369  24385-5  20540-2 0  9990
2 44487  97.3640 135.4831 0008513 270.7756  89.2560 16.25055223305249
Epoch: 2025-02-19T04:13Z
TLE epoch observation values (Epoch: 2025-02-19T04:13:30.284Z)
Latitude
-0.00004°
Longitude
-77.26288°
Altitude
209.027 km
Speed
7.781 km/s
True Right ascension
09h 01m 55s
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
03:06:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
208.29 km
Perigee altitude
197.085 km
Semi-major axis
6,580.824 km
Eccentricity
0.00085
Inclination
97.364°
RAAN
135.4831°
Arg. of periapsis
270.7756°
True anomaly
89.35354°
Mean anomaly
89.256°
Eccentric anomaly
89.30477°
Mean motion
4.06558 °/min
Orbital period
88.55 mins
BSTAR
0.002054
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Other satellites on launch #52 in the year 2019 (2019-08-17 UTC)

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