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 | 9 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 9 hours ago
0 SPACEMOBILE-002
1 61048U 24163D 25040.23404949 .00006322 00000-0 30983-3 0 9990
2 61048 52.9743 55.1978 0012372 68.2614 291.9695 15.19342384 22766
Epoch: 2025-02-09T05:37Z
Definitive object data (Epoch: 2025-02-09T05:37:01.875Z)
Latitude | -0.00007° |
Longitude | -168.63057° |
Altitude | 505.524 km |
Speed | 7.614 km/s |
True Right ascension | 03h 40m 47s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -48.83871° |
Longitude | 130.52178° |
Altitude | 531.063 km |
Speed | 7.594 km/s |
Apparent Right ascension | 02h 29m 03s |
Apparent Declination | -52° 22' 52" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 17:06:12 |
Azimuth | 128.22° SE |
Elevation | -60.53° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 516.632 km |
Perigee altitude | 499.592 km |
Semi-major axis | 6,886.249 km |
Eccentricity | 0.0012372 |
Inclination | 52.9743° |
RAAN | 55.1978° |
Arg. of periapsis | 68.2614° |
True anomaly | 291.83795° |
Mean anomaly | 291.9695° |
Eccentric anomaly | 291.90373° |
Mean motion | 3.79812 °/min |
BSTAR | 0.00030983 |
Orbital period | 94.78 mins |
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Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
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 | 2025-02-10 02:17:53.164Z | 158.98° S | 2025-02-10 02:19:53.164Z | 123.285° SE | 15.747° | 2025-02-10 02:21:53.164Z | 90.207° ESE |
5 mins | 2025-02-10 03:55:53.164Z | 249.374° W | 2025-02-10 03:57:53.164Z | 317.32° NNW | 41.198° | 2025-02-10 04:00:53.164Z | 41.898° NE |
5 mins | 2025-02-10 08:54:53.164Z | 342.458° N | 2025-02-10 08:56:53.164Z | 23.317° NE | 21.398° | 2025-02-10 08:59:53.164Z | 77.709° E |
5 mins | 2025-02-10 10:33:53.164Z | 297.647° NW | 2025-02-10 10:35:53.164Z | 221.453° SW | 42.168° | 2025-02-10 10:38:53.164Z | 143.137° SSE |
Authenticating...
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