SPACEMOBILE-005, 61046
Orbit data source: Space-Track
SPACEMOBILE-005, 61046 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.
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61046 intel report
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SPACEMOBILE-005 radio frequencies
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SPACEMOBILE-005 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 12 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 12 hours ago
0 SPACEMOBILE-005
1 61046U 24163B 24288.11269488 .00003577 00000-0 19120-3 0 9994
2 61046 52.9756 236.6598 0014338 61.6507 298.5930 15.17560391 4813Epoch: 2024-10-14T02:42Z
Definitive object data (Epoch: 2024-10-14T02:42:16.837Z)
| Latitude | -0.00002° |
| Longitude | 172.94513° |
| Altitude | 509.374 km |
| Speed | 7.613 km/s |
| True Right ascension | 15h 46m 38s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | 32.93849° |
| Longitude | -38.35457° |
| Altitude | 512.66 km |
| Speed | 7.613 km/s |
| Apparent Right ascension | 23h 32m 29s |
| Apparent Declination | -2° 15' 49" |
| Sunlit | Object is in full shadow |
Predictive observer data (real-time)
| Local Sidereal Time | 08:56:11 |
| Azimuth | 306.583° NW |
| Elevation | -38.339° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 523.382 km |
| Perigee | 503.62 km |
| Semi-major axis | 6,891.638 km |
| Eccentricity | 0.0014338 |
| Inclination | 52.9756° |
| RAAN | 236.6598° |
| Arg. of periapsis | 61.6507° |
| True anomaly | 298.44861° |
| Mean anomaly | 298.593° |
| Eccentric anomaly | 298.52082° |
| Mean motion | 3.79367 °/min |
| BSTAR | 0.0001912 |
| 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-005 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 23:26:10.373Z | 227.524° WSW | 2024-10-14 23:29:10.373Z | 85.239° E | 44.83° | 2024-10-14 23:32:10.373Z | 51.269° ENE |
| 6 mins | 2024-10-15 06:05:10.373Z | 313.254° NW | 2024-10-15 06:07:10.373Z | 337.32° NNW | 43.511° | 2024-10-15 06:11:10.373Z | 127.111° SE |