LT-1 O1A, 51284
Orbit data source: Space-Track
LT-1 O1A, 51284 is a payload satellite owned by SAST (CN) in SSO that was launched on Tue, 25 Jan 2022 UTC via a CHANG ZHENG 4C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payloads include a variety of satellites, spacecraft, and rockets 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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51284 intel report (Beta)
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LT-1 O1A details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 7 hours ago |
| Origin | |
| Manufacturer | SAST |
| Mission | Operational Civil Radar Imaging |
| Bus & Motor | LSAR, AOCS 20N |
| Mass | 3,200 kg wet, ~2,500 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 4 Pan, 10 m |
| Radar Cross Section | 14.608 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 7 hours ago
0 LT-1 O1A
1 51284U 22007A 24303.95426662 .00003736 00000-0 40873-3 0 9997
2 51284 97.8105 308.9203 0001611 93.0150 267.1252 14.88419931149933Epoch: 2024-10-29T22:54Z
Definitive object data (Epoch: 2024-10-29T22:54:08.635Z)
| Latitude | 0.00003° |
| Longitude | -73.37439° |
| Altitude | 605.964 km |
| Speed | 7.556 km/s |
| True Right ascension | 20h 35m 40s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -20.20896° |
| Longitude | 104.04891° |
| Altitude | 610.984 km |
| Speed | 7.552 km/s |
| Apparent Right ascension | 10h 39m 42s |
| Apparent Declination | -36° 27' 58" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 01:50:55 |
| Azimuth | 100.391° ESE |
| Elevation | -52.717° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 601.022 km |
| Perigee | 598.773 km |
| Semi-major axis | 6,978.034 km |
| Eccentricity | 0.0001611 |
| Inclination | 97.8105° |
| RAAN | 308.9203° |
| Arg. of periapsis | 93.015° |
| True anomaly | 267.10676° |
| Mean anomaly | 267.1252° |
| Eccentric anomaly | 267.11598° |
| Mean motion | 3.72343 °/min |
| BSTAR | 0.00040873 |
| Period | 96.68 mins |
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Other satellites on launch #7 in the year 2022 (2022-01-25 UTC)
| LT-1 O1A, 51284 |
| CZ-4C R/B, 51285 |
| CZ-4C DEB, 51286 (Decayed) |
LT-1 O1A 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-10-30 12:24:09.298Z | 55.1° ENE | 2024-10-30 12:26:09.298Z | 86.047° E | 17.078° | 2024-10-30 12:29:09.298Z | 134.19° SE |
| 6 mins | 2024-10-30 14:00:09.298Z | 341.109° N | 2024-10-30 14:02:09.298Z | 297.19° NW | 29.643° | 2024-10-30 14:06:09.298Z | 223.645° SW |
| 6 mins | 2024-10-31 00:51:09.298Z | 190.12° SSW | 2024-10-31 00:54:09.298Z | 287.066° WNW | 37.518° | 2024-10-31 00:57:09.298Z | 335.454° NNW |