CENTAURI-6, 59451
Orbit data source: Space-Track
CENTAURI-6, 59451 is a payload satellite owned by Fleet Space (AU) 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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59451 intel report (Beta)
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CENTAURI-6 radio frequencies
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CENTAURI-6 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 9 hours ago |
| Origin | |
| Manufacturer | Terran Orbital |
| Mission | Operational spacecraft |
| Bus & Motor | CUBESAT 12U, Unknown motor |
| Mass | ~20 kg wet, ~20 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Medium (>0.1 m² and <1 m²) |
Expand to show TLE details & history
TLE from 9 hours ago
0 CENTAURI-6
1 59451U 24066K 24296.57777365 .00008080 00000-0 72799-3 0 9995
2 59451 45.6042 141.3750 0003292 148.2880 211.8198 14.96061391 29545Epoch: 2024-10-22T13:51Z
Definitive object data (Epoch: 2024-10-22T13:51:59.643Z)
| Latitude | -0.00007° |
| Longitude | -98.11166° |
| Altitude | 581.092 km |
| Speed | 7.57 km/s |
| True Right ascension | 09h 25m 29s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 20.0218° |
| Longitude | 59.24142° |
| Altitude | 576.415 km |
| Speed | 7.577 km/s |
| Apparent Right ascension | 23h 06m 16s |
| Apparent Declination | -24° 55' 11" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 17:40:06 |
| Azimuth | 114.499° SE |
| Elevation | -9.673° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 582.858 km |
| Perigee | 578.276 km |
| Semi-major axis | 6,958.704 km |
| Eccentricity | 0.0003292 |
| Inclination | 45.6042° |
| RAAN | 141.375° |
| Arg. of periapsis | 148.288° |
| True anomaly | 211.79992° |
| Mean anomaly | 211.8198° |
| Eccentric anomaly | 211.80986° |
| Mean motion | 3.73896 °/min |
| BSTAR | 0.00072799 |
| Period | 96.28 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 |
CENTAURI-6 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 | 2024-10-23 00:01:12.422Z | 266.903° W | 2024-10-23 00:04:12.422Z | 214.975° SW | 21.365° | 2024-10-23 00:07:12.422Z | 168.825° S |
| 4 mins | 2024-10-23 15:41:12.422Z | 165.511° S | 2024-10-23 15:43:12.422Z | 131.59° SE | 16.978° | 2024-10-23 15:45:12.422Z | 101.044° ESE |
| 7 mins | 2024-10-23 17:20:12.422Z | 239.411° WSW | 2024-10-23 17:23:12.422Z | 186.132° SSW | 44.646° | 2024-10-23 17:27:12.422Z | 66.306° ENE |
| 6 mins | 2024-10-23 19:02:12.422Z | 293.061° NW | 2024-10-23 19:04:12.422Z | 340.217° N | 33.199° | 2024-10-23 19:08:12.422Z | 61.227° ENE |
| 6 mins | 2024-10-23 20:43:12.422Z | 306.079° NW | 2024-10-23 20:46:12.422Z | 21.603° NNE | 34.376° | 2024-10-23 20:49:12.422Z | 79.314° E |
| 7 mins | 2024-10-23 22:24:12.422Z | 289.316° WNW | 2024-10-23 22:27:12.422Z | 189.881° SSW | 43.192° | 2024-10-23 22:31:12.422Z | 125.601° SE |