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 (Beta)
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SPACEMOBILE-005 radio frequencies
SPACEMOBILE-005 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-005
1 61046U 24163B 24346.44168839 .00008157 00000-0 40290-3 0 9994
2 61046 52.9788 329.5601 0010350 235.2212 124.7807 15.18686429 13676Epoch: 2024-12-11T10:36Z
Definitive object data (Epoch: 2024-12-11T10:36:01.876Z)
| Latitude | -0.0001° |
| Longitude | 89.91588° |
| Altitude | 514.757 km |
| Speed | 7.605 km/s |
| True Right ascension | 21h 58m 14s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -11.12544° |
| Longitude | 77.8259° |
| Altitude | 515.012 km |
| Speed | 7.605 km/s |
| Apparent Right ascension | 19h 02m 14s |
| Apparent Declination | -30° 40' 40" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 03:54:43 |
| Azimuth | 268.713° W |
| Elevation | -51.103° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 517.223 km |
| Perigee altitude | 502.965 km |
| Semi-major axis | 6,888.231 km |
| Eccentricity | 0.001035 |
| Inclination | 52.9788° |
| RAAN | 329.5601° |
| Arg. of periapsis | 235.2212° |
| True anomaly | 124.87804° |
| Mean anomaly | 124.7807° |
| Eccentric anomaly | 124.82938° |
| Mean motion | 3.79648 °/min |
| BSTAR | 0.0004029 |
| Orbital period | 94.82 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-005 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 07:36:32.733Z | 337.709° N | 2024-12-12 07:38:32.733Z | 22.725° NE | 27.15° | 2024-12-12 07:41:32.733Z | 87.486° E |
| 5 mins | 2024-12-12 09:15:32.733Z | 282.009° WNW | 2024-12-12 09:17:32.733Z | 224.379° SW | 32.571° | 2024-12-12 09:20:32.733Z | 160.119° S |
| 5 mins | 2024-12-13 00:40:32.733Z | 176.256° S | 2024-12-13 00:42:32.733Z | 129.207° SE | 25.66° | 2024-12-13 00:45:32.733Z | 73.369° E |
| 6 mins | 2024-12-13 02:18:32.733Z | 265.62° W | 2024-12-13 02:21:32.733Z | 346.955° N | 31.367° | 2024-12-13 02:24:32.733Z | 37.172° NE |
Authenticating...
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