OBJECT G, 43668 (Decayed)
Orbit data source: Space-Track
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT G, 43668 was a satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Mon, 29 Oct 2018 UTC via a CHANG ZHENG 2C 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.
43668 intel report (Beta)
OBJECT G details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 4 months ago |
| Origin | |
| Manufacturer | GUOG? |
| Mission | Decayed Commercial Communications |
| Bus & Motor | CUBESAT 6U?, Unknown motor |
| Mass | 8 kg wet, 8 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box, 0.3 m |
| Radar Cross Section | 0.080 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 4 months ago
0 OBJECT G
1 43668U 18083G 24242.60640799 .17607915 25949-5 18972-3 0 9992
2 43668 97.3019 279.9083 0012410 225.0961 134.9337 16.50034885324963Definitive object data (Epoch: 2024-08-29T14:33:13.65Z)
| Latitude | -0.00009° |
| Longitude | 83.31009° |
| Altitude | 148.23 km |
| Speed | 7.814 km/s |
| True Right ascension | 18h 39m 37s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow 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 altitude | 144.118 km |
| Perigee altitude | 127.95 km |
| Semi-major axis | 6,514.171 km |
| Eccentricity | 0.001241 |
| Inclination | 97.3019° |
| RAAN | 279.9083° |
| Arg. of periapsis | 225.0961° |
| True anomaly | 135.03426° |
| Mean anomaly | 134.9337° |
| Eccentric anomaly | 134.98399° |
| Mean motion | 4.12814 °/min |
| BSTAR | 0.00018972 |
| Orbital period | 87.21 mins |
Other satellites on launch #83 in the year 2018 (2018-10-29 UTC)
| CFOSAT, 43662 |
| OBJECT B, 43663 (Decayed) |
| OBJECT C, 43664 |
| OBJECT D, 43665 |
| OBJECT E, 43666 (Decayed) |
| CZ-2C R/B, 43667 (Decayed) |
| OBJECT G, 43668 (Decayed) |
| OBJECT H, 43669 (Decayed) |
OBJECT G Visibility forecast
Observer location: undefined°, undefined
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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