OBJECT F, 44315 (Decayed)
Orbit data source: Space-Track
OBJECT F, 44315 was a Chinese satellite in LEO that was launched on Wed, 05 Jun 2019 UTC via a CHANG ZHENG 11 launch vehicle from the Yellow Sea Launch Area, China (YSLA). 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.
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44315 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
2.000 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 OBJECT F
1 44315U 19032F 26116.08672172 .07634054 10452-4 95146-3 0 9994
2 44315 44.9557 153.4418 0002336 17.0554 343.0447 16.35144130381404Epoch: 2026-04-26T02:04Z
TLE epoch observation values (Epoch: 2026-04-26T02:04:52.756Z)
Latitude
-0.00006°
Longitude
-91.87386°
Altitude
177.28 km
Speed
7.803 km/s
True Right ascension
10h 13m 46s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
00:51:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
181.975 km
Perigee altitude
178.911 km
Semi-major axis
6,558.58 km
Eccentricity
0.00023
Inclination
44.9557°
RAAN
153.4418°
Arg. of periapsis
17.0554°
True anomaly
343.03689°
Mean anomaly
343.0447°
Eccentric anomaly
343.0408°
Mean motion
4.08628 °/min
Orbital period
88.1 mins
BSTAR
0.00095146
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Other satellites on launch #32 in the year 2019 (2019-06-05 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT F Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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