OBJECT E, 44314
Orbit data source: Space-Track
OBJECT E, 44314 is a payload satellite owned by CAST (CN) 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). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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44314 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 OBJECT E
1 44314U 19032E 26317.92434595 .00016491 00000-0 36697-3 0 9996
2 44314 44.9987 225.5824 0009890 146.2921 213.8598 15.43455551411176TLE epoch observation values (Epoch: 2026-11-13T22:11:03.490Z)
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Visualization observer readout
Orbital elements
Other satellites on launch #32 in the year 2019 (2019-06-05 UTC)
OBJECT E Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-14 03:19:38.761Z | 280.795° WNW | 2026-11-14 03:22:38.761Z | 192.958° SSW | 42.485° | 2026-11-14 03:24:38.761Z | 144.258° SSE |
| 5 mins | 2026-11-14 21:43:38.761Z | 241.945° WSW | 2026-11-14 21:45:38.761Z | 115.153° SE | 83.149° | 2026-11-14 21:48:38.761Z | 67.181° ENE |
| 5 mins | 2026-11-14 23:21:38.761Z | 296.911° NW | 2026-11-14 23:23:38.761Z | 358.266° N | 35.974° | 2026-11-14 23:26:38.761Z | 60.94° ENE |
| 5 mins | 2026-11-15 00:59:38.761Z | 309.598° NW | 2026-11-15 01:01:38.761Z | 8.846° NNE | 40.199° | 2026-11-15 01:04:38.761Z | 81.044° E |
| 5 mins | 2026-11-15 02:37:38.761Z | 281.704° WNW | 2026-11-15 02:39:38.761Z | 196.377° SSW | 59.649° | 2026-11-15 02:42:38.761Z | 128.9° SE |
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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