NUSAT-3, 42760
Orbit data source: Space-Track
NUSAT-3, 42760 is a payload satellite owned by URUGUS S.A. (AR) in LEO that was launched on Thu, 15 Jun 2017 UTC via a CHANG ZHENG 4B 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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42760 intel report (Beta)
NUSAT-3 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 7 hours ago |
| Origin | |
| Manufacturer | URUGUS S.A. |
| Mission | Operational Commercial Imaging |
| Bus & Motor | ALEPH, Unknown motor |
| Mass | 37 kg wet, 37 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box, 0.75 m |
| Radar Cross Section | 0.380 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 7 hours ago
0 NUSAT-3
1 42760U 17034C 24361.55466940 .00061576 00000-0 11084-2 0 9990
2 42760 43.0021 187.2507 0020153 250.4942 109.3741 15.48748450417225Epoch: 2024-12-26T13:18Z
Definitive object data (Epoch: 2024-12-26T13:18:43.436Z)
| Latitude | 0.00002° |
| Longitude | -107.96265° |
| Altitude | 424.729 km |
| Speed | 7.656 km/s |
| True Right ascension | 12h 29m 00s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 41.10161° |
| Longitude | -41.06762° |
| Altitude | 436.662 km |
| Speed | 7.648 km/s |
| Apparent Right ascension | 12h 22m 31s |
| Apparent Declination | 7° 31' 08" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 19:12:01 |
| Azimuth | 283.735° WNW |
| Elevation | -4.53° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 436.054 km |
| Perigee altitude | 408.644 km |
| Semi-major axis | 6,800.486 km |
| Eccentricity | 0.0020153 |
| Inclination | 43.0021° |
| RAAN | 187.2507° |
| Arg. of periapsis | 250.4942° |
| True anomaly | 109.59178° |
| Mean anomaly | 109.3741° |
| Eccentric anomaly | 109.48296° |
| Mean motion | 3.8702 °/min |
| BSTAR | 0.0011084 |
| Orbital period | 93.02 mins |
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Other satellites on launch #34 in the year 2017 (2017-06-15 UTC)
| HXMT, 42758 |
| ZHUHAI-1 02, 42759 |
| NUSAT-3, 42760 |
| ZHUHAI-1 01, 42761 |
| CZ-4B R/B, 42762 (Decayed) |
| CZ-4B DEB, 43430 |
| CZ-4B DEB, 43431 |
NUSAT-3 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2024-12-26 19:53:17.711Z | 291.108° WNW | 2024-12-26 19:56:17.711Z | 13.889° NNE | 40.245° | 2024-12-26 19:59:17.711Z | 89.37° E |
| 4 mins | 2024-12-26 21:32:17.711Z | 263.889° W | 2024-12-26 21:33:17.711Z | 233.594° WSW | 33.446° | 2024-12-26 21:36:17.711Z | 137.665° SSE |
| 4 mins | 2024-12-27 15:51:17.711Z | 204.902° SW | 2024-12-27 15:53:17.711Z | 129.601° SE | 31.023° | 2024-12-27 15:55:17.711Z | 87.017° E |
| 5 mins | 2024-12-27 17:28:17.711Z | 272.85° WNW | 2024-12-27 17:30:17.711Z | 347.844° N | 41.313° | 2024-12-27 17:33:17.711Z | 68.984° E |
| 5 mins | 2024-12-27 19:06:17.711Z | 298.807° NW | 2024-12-27 19:08:17.711Z | 20.679° NNE | 37.767° | 2024-12-27 19:11:17.711Z | 83.491° E |
Authenticating...
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