SPACEMOBILE-002, 61048
Orbit data source: Space-Track
SPACEMOBILE-002, 61048 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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61048 intel report (Beta)
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SPACEMOBILE-002 radio frequencies
SPACEMOBILE-002 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 1 day 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 1 day ago
0 SPACEMOBILE-002
1 61048U 24163D 24346.15895860 .00006883 00000-0 34270-3 0 9990
2 61048 52.9727 330.6312 0010002 235.7047 124.3000 15.18658151 13636Epoch: 2024-12-11T03:48Z
Definitive object data (Epoch: 2024-12-11T03:48:54.023Z)
| Latitude | 0.00001° |
| Longitude | -166.95154° |
| Altitude | 514.657 km |
| Speed | 7.605 km/s |
| True Right ascension | 22h 02m 31s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 35.0702° |
| Longitude | -139.73768° |
| Altitude | 519.139 km |
| Speed | 7.605 km/s |
| Apparent Right ascension | 19h 51m 53s |
| Apparent Declination | -2° 19' 14" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 02:07:20 |
| Azimuth | 270.699° WNW |
| Elevation | -4.453° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 517.07 km |
| Perigee altitude | 503.291 km |
| Semi-major axis | 6,888.317 km |
| Eccentricity | 0.0010002 |
| Inclination | 52.9727° |
| RAAN | 330.6312° |
| Arg. of periapsis | 235.7047° |
| True anomaly | 124.39462° |
| Mean anomaly | 124.3° |
| Eccentric anomaly | 124.34731° |
| Mean motion | 3.79641 °/min |
| BSTAR | 0.0003427 |
| Orbital period | 94.83 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-002 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2024-12-12 03:47:27.855Z | 305.18° NW | 2024-12-12 03:49:27.855Z | 340.428° N | 17.111° | 2024-12-12 03:51:27.855Z | 16.026° NNE |
| 4 mins | 2024-12-12 07:07:27.855Z | 345.087° N | 2024-12-12 07:09:27.855Z | 25.795° NE | 20.65° | 2024-12-12 07:11:27.855Z | 64.871° ENE |
| 5 mins | 2024-12-12 08:46:27.855Z | 302.098° NW | 2024-12-12 08:48:27.855Z | 213.888° SW | 43.893° | 2024-12-12 08:51:27.855Z | 138.343° SSE |
| 6 mins | 2024-12-13 01:49:27.855Z | 244.901° WSW | 2024-12-13 01:51:27.855Z | 287.231° WNW | 41.027° | 2024-12-13 01:55:27.855Z | 44.981° NE |
Authenticating...
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