SPACEMOBILE-004, 61049
Orbit data source: Space-Track
SPACEMOBILE-004, 61049 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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61049 intel report (Beta)
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SPACEMOBILE-004 radio frequencies
SPACEMOBILE-004 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 23 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 23 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 24346.27770195 .00006983 00000-0 34680-3 0 9993
2 61049 52.9751 329.9589 0010139 248.7936 111.1975 15.18724994 13659Epoch: 2024-12-11T06:39Z
Definitive object data (Epoch: 2024-12-11T06:39:53.448Z)
| Latitude | 0.00002° |
| Longitude | 149.51153° |
| Altitude | 513.1 km |
| Speed | 7.607 km/s |
| True Right ascension | 21h 59m 50s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -1.46101° |
| Longitude | -33.76902° |
| Altitude | 508.336 km |
| Speed | 7.612 km/s |
| Apparent Right ascension | 12h 12m 43s |
| Apparent Declination | -27° 18' 37" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 03:59:37 |
| Azimuth | 93.01° ESE |
| Elevation | -41.939° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 516.962 km |
| Perigee altitude | 502.994 km |
| Semi-major axis | 6,888.115 km |
| Eccentricity | 0.0010139 |
| Inclination | 52.9751° |
| RAAN | 329.9589° |
| Arg. of periapsis | 248.7936° |
| True anomaly | 111.30577° |
| Mean anomaly | 111.1975° |
| Eccentric anomaly | 111.25164° |
| Mean motion | 3.79658 °/min |
| BSTAR | 0.0003468 |
| 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-004 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 06:47:25.784Z | 338.403° N | 2024-12-12 06:49:25.784Z | 11.385° NNE | 17.375° | 2024-12-12 06:52:25.784Z | 63.361° ENE |
| 6 mins | 2024-12-12 08:26:25.784Z | 314.61° NW | 2024-12-12 08:29:25.784Z | 88.825° E | 42.865° | 2024-12-12 08:32:25.784Z | 124.175° SE |
| 6 mins | 2024-12-13 01:29:25.784Z | 227.569° WSW | 2024-12-13 01:32:25.784Z | 142.615° SSE | 44.945° | 2024-12-13 01:35:25.784Z | 51.286° ENE |
| 4 mins | 2024-12-13 03:10:25.784Z | 314.143° NW | 2024-12-13 03:11:25.784Z | 335.098° NNW | 19.383° | 2024-12-13 03:14:25.784Z | 26.706° NE |
Authenticating...
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