EUROPA CLIPPER, 61507
Orbit data source: Space-Track
EUROPA CLIPPER, 61507 is a payload satellite owned by JPL (US) in LEO that was launched on Mon, 14 Oct 2024 UTC via an FALCON HEAVY 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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61507 intel report (Beta)
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EUROPA CLIPPER details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 1 week ago |
| Origin | |
| Manufacturer | JPL |
| Mission | Operational spacecraft |
| Bus & Motor | EUROPA, AOCS |
| Mass | 5,700 kg wet, 3,241 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | RCS unknown |
Expand to show TLE details & history
TLE from 1 week ago
0 EUROPA CLIPPER
1 61507U 24182A 24288.67632810 .00000840 -26562-5 00000-0 0 9992
2 61507 31.9400 67.0176 0018900 60.7600 70.5300 16.38814738 06Epoch: 2024-10-14T16:13Z
Definitive object data (Epoch: 2024-10-14T16:13:54.747Z)
| Latitude | 23.45054° |
| Longitude | -63.93444° |
| Altitude | 163.258 km |
| Speed | 7.816 km/s |
| True Right ascension | 13h 32m 58s |
| True Declination | 23° 18' 50" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -29.92494° |
| Longitude | -16.78571° |
| Altitude | 176.099 km |
| Speed | 7.802 km/s |
| Apparent Right ascension | 20h 15m 29s |
| Apparent Declination | -77° 33' 20" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 15:40:05 |
| Azimuth | 165.879° S |
| Elevation | -34.538° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 185.247 km |
| Perigee | 160.485 km |
| Semi-major axis | 6,551.003 km |
| Eccentricity | 0.00189 |
| Inclination | 31.94° |
| RAAN | 67.0176° |
| Arg. of periapsis | 60.76° |
| True anomaly | 70.73435° |
| Mean anomaly | 70.53° |
| Eccentric anomaly | 70.63216° |
| Mean motion | 4.09337 °/min |
| BSTAR | Unknown |
| Period | 87.95 mins |
No data available
No data available
Other satellites on launch #182 in the year 2024 (2024-10-14 UTC)
| EUROPA CLIPPER, 61507 |
| FALCON HEAVY R/B, 61508 |
EUROPA CLIPPER Visibility forecast
Observer location: 39.9160978°, -105.1181434
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. |
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