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 | 7 hours ago |
| Origin | |
| Manufacturer | AST & Science |
| Mission | Operational Commercial Communications |
| 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 | Box + 1 Plate, 9 m |
| Radar Cross Section | 1.500 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 7 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 25045.34921916 .00007209 00000-0 35025-3 0 9993
2 61049 52.9739 31.5643 0012502 88.4462 271.7963 15.19429552 23543Epoch: 2025-02-14T08:22Z
Definitive object data (Epoch: 2025-02-14T08:22:52.535Z)
| Latitude | -0.00007° |
| Longitude | 121.23309° |
| Altitude | 508.18 km |
| Speed | 7.611 km/s |
| True Right ascension | 02h 06m 15s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 17.78819° |
| Longitude | -74.03212° |
| Altitude | 504.634 km |
| Speed | 7.616 km/s |
| Apparent Right ascension | 10h 16m 58s |
| Apparent Declination | -15° 42' 55" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 18:02:13 |
| Azimuth | 274.377° WNW |
| Elevation | -30.07° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 516.458 km |
| Perigee altitude | 499.24 km |
| Semi-major axis | 6,885.986 km |
| Eccentricity | 0.0012502 |
| Inclination | 52.9739° |
| RAAN | 31.5643° |
| Arg. of periapsis | 88.4462° |
| True anomaly | 271.6531° |
| Mean anomaly | 271.7963° |
| Eccentric anomaly | 271.7247° |
| Mean motion | 3.79834 °/min |
| BSTAR | 0.00035025 |
| Orbital period | 94.78 mins |
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Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
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 | 2025-02-15 01:57:06.110Z | 240.841° WSW | 2025-02-15 01:59:06.110Z | 301.571° NW | 43.458° | 2025-02-15 02:02:06.110Z | 45.122° ENE |
| 5 mins | 2025-02-15 08:35:06.110Z | 304.331° NW | 2025-02-15 08:37:06.110Z | 233.458° WSW | 44.316° | 2025-02-15 08:40:06.110Z | 136.608° SSE |
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