SPACEMOBILE-003, 61045
Orbit data source: Space-Track
SPACEMOBILE-003, 61045 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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61045 intel report (Beta)
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SPACEMOBILE-003 radio frequencies
SPACEMOBILE-003 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 14 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 14 hours ago
0 SPACEMOBILE-003
1 61045U 24163A 24346.65270130 .00006681 00000-0 33498-3 0 9996
2 61045 52.9786 328.7220 0010101 231.1487 128.8605 15.18461077 13710Epoch: 2024-12-11T15:39Z
Definitive object data (Epoch: 2024-12-11T15:39:53.392Z)
| Latitude | -0.00005° |
| Longitude | 12.90519° |
| Altitude | 515.737 km |
| Speed | 7.605 km/s |
| True Right ascension | 21h 54m 53s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -52.50447° |
| Longitude | -91.88597° |
| Altitude | 522.639 km |
| Speed | 7.605 km/s |
| Apparent Right ascension | 15h 26m 13s |
| Apparent Declination | -46° 29' 42" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 03:52:24 |
| Azimuth | 146.249° SSE |
| Elevation | -81.879° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 517.734 km |
| Perigee altitude | 503.817 km |
| Semi-major axis | 6,888.912 km |
| Eccentricity | 0.0010101 |
| Inclination | 52.9786° |
| RAAN | 328.722° |
| Arg. of periapsis | 231.1487° |
| True anomaly | 128.95056° |
| Mean anomaly | 128.8605° |
| Eccentric anomaly | 128.90554° |
| Mean motion | 3.79592 °/min |
| BSTAR | 0.00033498 |
| Orbital period | 94.84 mins |
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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-003 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 | 2024-12-12 07:57:14.352Z | 333.189° NNW | 2024-12-12 07:59:14.352Z | 27.982° NE | 33.674° | 2024-12-12 08:02:14.352Z | 100.341° ESE |
| 4 mins | 2024-12-12 09:36:14.352Z | 268.072° W | 2024-12-12 09:38:14.352Z | 220.443° SW | 23.476° | 2024-12-12 09:40:14.352Z | 181.285° SSW |
| 5 mins | 2024-12-13 01:01:14.352Z | 191.238° SSW | 2024-12-13 01:03:14.352Z | 124.991° SE | 34.604° | 2024-12-13 01:06:14.352Z | 64.669° ENE |
| 5 mins | 2024-12-13 02:40:14.352Z | 290.656° WNW | 2024-12-13 02:42:14.352Z | 342.899° N | 25.784° | 2024-12-13 02:45:14.352Z | 33.255° NE |
Authenticating...
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