OBJECT E, 43835
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, 43835 is a satellite in SSO that was launched on Fri, 07 Dec 2018 UTC via a CHANG ZHENG 2D 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.
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43835 intel report (Beta)
OBJECT E details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 7 hours ago |
| Origin | |
| Manufacturer | GUOX/CTYK |
| Mission | Commercial Communications |
| Bus & Motor | CUBESAT 3U, 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 7 hours ago
0 OBJECT E
1 43835U 18102E 24361.12290925 .00211275 00000-0 17496-2 0 9998
2 43835 97.4124 83.8995 0004558 196.0886 164.0231 15.69588617334984Epoch: 2024-12-26T02:56Z
Definitive object data (Epoch: 2024-12-26T02:56:59.359Z)
| Latitude | -0.00009° |
| Longitude | -55.45465° |
| Altitude | 366.185 km |
| Speed | 7.688 km/s |
| True Right ascension | 05h 35m 35s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -71.00637° |
| Longitude | 102.78557° |
| Altitude | 384.446 km |
| Speed | 7.679 km/s |
| Apparent Right ascension | 19h 59m 56s |
| Apparent Declination | -61° 21' 37" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 09:29:37 |
| Azimuth | 154.818° SSE |
| Elevation | -64.552° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 360.044 km |
| Perigee altitude | 353.905 km |
| Semi-major axis | 6,735.111 km |
| Eccentricity | 0.0004558 |
| Inclination | 97.4124° |
| RAAN | 83.8995° |
| Arg. of periapsis | 196.0886° |
| True anomaly | 164.03747° |
| Mean anomaly | 164.0231° |
| Eccentric anomaly | 164.03029° |
| Mean motion | 3.92668 °/min |
| BSTAR | 0.0017496 |
| Orbital period | 91.68 mins |
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Other satellites on launch #102 in the year 2018 (2018-12-07 UTC)
OBJECT E 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2024-12-26 18:48:29.575Z | 0.46° NNE | 2024-12-26 18:50:29.575Z | 278.747° WNW | 40.522° | 2024-12-26 18:52:29.575Z | 206.894° SW |
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