SPACEMOBILE-001, 61047
Orbit data source: Space-Track
SPACEMOBILE-001, 61047 is a payload satellite owned by AST & Science (US) in LEO that was launched on Thu, 12 Sep 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.
Focus sentinelFocus sentinel
61047 intel report
Focus sentinelFocus sentinel
SPACEMOBILE-001 radio frequencies
Loading greatness...
SPACEMOBILE-001 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 19 hours ago |
| Origin | |
| Manufacturer | AST & Science |
| Mission | Operational spacecraft |
| Bus & Motor | BW3, Unknown motor |
| Mass | 1,500 kg wet, 1,500 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 19 hours ago
0 SPACEMOBILE-001
1 61047U 24163C 24287.84829593 .00003619 00000-0 19302-3 0 9992
2 61047 52.9722 237.8381 0014088 61.8422 298.3993 15.17608970 4778Epoch: 2024-10-13T20:21Z
Definitive object data (Epoch: 2024-10-13T20:21:32.768Z)
| Latitude | 0.00004° |
| Longitude | -90.4323° |
| Altitude | 509.337 km |
| Speed | 7.613 km/s |
| True Right ascension | 15h 51m 21s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | 27.07149° |
| Longitude | -71.53403° |
| Altitude | 505.846 km |
| Speed | 7.62 km/s |
| Apparent Right ascension | 19h 15m 36s |
| Apparent Declination | -6° 09' 56" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 10:02:49 |
| Azimuth | 59.321° ENE |
| Elevation | -39.594° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 523.063 km |
| Perigee | 503.646 km |
| Semi-major axis | 6,891.492 km |
| Eccentricity | 0.0014088 |
| Inclination | 52.9722° |
| RAAN | 237.8381° |
| Arg. of periapsis | 61.8422° |
| True anomaly | 298.25717° |
| Mean anomaly | 298.3993° |
| Eccentric anomaly | 298.32825° |
| Mean motion | 3.79379 °/min |
| BSTAR | 0.00019302 |
| Period | 94.89 mins |
No data available
No data available
Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
| SPACEMOBILE-003, 61045 |
| SPACEMOBILE-005, 61046 |
| SPACEMOBILE-001, 61047 |
| SPACEMOBILE-002, 61048 |
| SPACEMOBILE-004, 61049 |
SPACEMOBILE-001 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2024-10-14 23:24:37.132Z | 226.428° WSW | 2024-10-14 23:27:37.132Z | 118.303° SE | 44.822° | 2024-10-14 23:30:37.132Z | 51.917° ENE |
| 4 mins | 2024-10-15 01:05:37.132Z | 313.703° NW | 2024-10-15 01:06:37.132Z | 334.954° NNW | 19.162° | 2024-10-15 01:09:37.132Z | 26.935° NE |
| 6 mins | 2024-10-15 06:03:37.132Z | 313.976° NW | 2024-10-15 06:05:37.132Z | 339.638° N | 43.056° | 2024-10-15 06:09:37.132Z | 126.153° SE |