DECAYED

OBJECT E, 44842 (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 E, 44842 was a satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Sat, 07 Dec 2019 UTC via a KUAIZHOU-1A launch vehicle from the Taiyaun Space Center, China (TSC). 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
OBJECT E details
Identifier
44842, 2019-087E
Orbit
Decayed
Last TLE update8 months ago
Origin
Flag of CNGuodian Gaokeji (CN / PRC)
ManufacturerGUOG?
MissionDecayed Commercial Imaging
Bus & MotorCUBESAT 6U?, Unknown motor
Mass8 kg wet, 8 kg dry
Launch date (UTC)
2019-12-07 (5 years ago)
Launch vehicle
KUAIZHOU-1A
Launch site
Taiyaun Space Center, China (TSC)
Object typeUnknown
Shape & HBRBox, 0.3 m
Radar Cross Section0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 8 months ago
0 OBJECT E
1 44842U 19087E   24091.02873833  .07848714  25368-5  16623-2 0  9995
2 44842  97.4763 279.3477 0007439 271.5628  88.4815 16.30832210241101
Epoch: 2024-03-31T00:41Z
Definitive object data (Epoch: 2024-03-31T00:41:22.991Z)
Latitude0.00004°
Longitude80.11268°
Altitude193.415 km
Speed7.79 km/s
True Right ascension18h 37m 23s
True Declination0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.
Orbital elements
Apogee altitude192.011 km
Perigee altitude182.243 km
Semi-major axis6,565.264 km
Eccentricity0.0007439
Inclination97.4763°
RAAN279.3477°
Arg. of periapsis271.5628°
True anomaly88.56672°
Mean anomaly88.4815°
Eccentric anomaly88.52411°
Mean motion4.08004 °/min
BSTAR0.0016623
Orbital period88.23 mins
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OBJECT E Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
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