QPS-SAR-7 TSUKUYOMI-II, 59447
Orbit data source: Space-Track
QPS-SAR-7 TSUKUYOMI-II, 59447 is a payload satellite owned by QPS Labs (JP) in LEO that was launched on Sun, 07 Apr 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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59447 intel report (Beta)
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QPS-SAR-7 TSUKUYOMI-II details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 8 hours ago |
| Origin | |
| Manufacturer | QPS Labs |
| Mission | Operational spacecraft |
| Bus & Motor | QSAT, Unknown motor |
| Mass | ~120 kg wet, ~100 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 8 hours ago
0 QPS-SAR-7 TSUKUYOMI-II
1 59447U 24066F 24296.57665061 .00011059 00000-0 97824-3 0 9995
2 59447 45.6062 141.4341 0003084 166.8347 193.2614 14.96480660 29531Epoch: 2024-10-22T13:50Z
Definitive object data (Epoch: 2024-10-22T13:50:22.612Z)
| Latitude | -0.00004° |
| Longitude | -97.64713° |
| Altitude | 579.934 km |
| Speed | 7.571 km/s |
| True Right ascension | 09h 25m 44s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 42.87874° |
| Longitude | 15.8202° |
| Altitude | 580.099 km |
| Speed | 7.577 km/s |
| Apparent Right ascension | 12h 30m 12s |
| Apparent Declination | 45° 35' 56" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 17:26:47 |
| Azimuth | 302.29° NW |
| Elevation | 37.233° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 581.413 km |
| Perigee | 577.122 km |
| Semi-major axis | 6,957.405 km |
| Eccentricity | 0.0003084 |
| Inclination | 45.6062° |
| RAAN | 141.4341° |
| Arg. of periapsis | 166.8347° |
| True anomaly | 193.2533° |
| Mean anomaly | 193.2614° |
| Eccentric anomaly | 193.25735° |
| Mean motion | 3.74001 °/min |
| BSTAR | 0.00097824 |
| Period | 96.26 mins |
No data available
No data available
Other satellites on launch #66 in the year 2024 (2024-04-07 UTC)
| TSAT-1A, 59442 |
| HAWK-8A, 59443 |
| CAPELLA-14 (ACADIA), 59444 |
| HAWK-8B, 59445 |
| HAWK-9A, 59446 |
| QPS-SAR-7 TSUKUYOMI-II, 59447 |
| HAWK-9C, 59448 |
| HAWK-8C, 59449 |
| HAWK-9B, 59450 |
| CENTAURI-6, 59451 |
| OBJECT L, 59452 |
QPS-SAR-7 TSUKUYOMI-II 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 | 2024-10-22 22:19:55.434Z | 301.572° NW | 2024-10-22 22:21:55.434Z | 82.237° E | 43.487° | 2024-10-22 22:24:55.434Z | 110.459° ESE |
| 5 mins | 2024-10-22 23:59:55.434Z | 260.574° W | 2024-10-23 00:01:55.434Z | 223.92° SW | 21.988° | 2024-10-23 00:04:55.434Z | 171.692° S |
| 7 mins | 2024-10-23 17:17:55.434Z | 238.103° WSW | 2024-10-23 17:20:55.434Z | 194.079° SSW | 44.239° | 2024-10-23 17:24:55.434Z | 66.777° ENE |
| 6 mins | 2024-10-23 18:59:55.434Z | 291.722° WNW | 2024-10-23 19:01:55.434Z | 337.789° N | 33.282° | 2024-10-23 19:05:55.434Z | 60.758° ENE |
| 6 mins | 2024-10-23 20:40:55.434Z | 305.856° NW | 2024-10-23 20:43:55.434Z | 20.195° NNE | 34.131° | 2024-10-23 20:46:55.434Z | 78.374° E |