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 | 1 day 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 1 day ago
0 SPACEMOBILE-005
1 61046U 24163B 25042.48707064 .00007219 00000-0 35164-3 0 9993
2 61046 52.9790 45.0544 0013283 70.4407 289.8020 15.19328706 23109
Epoch: 2025-02-11T11:41Z
Definitive object data (Epoch: 2025-02-11T11:41:22.903Z)
Latitude | 0.00001° |
Longitude | 87.91779° |
Altitude | 505.656 km |
Speed | 7.614 km/s |
True Right ascension | 03h 00m 13s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 28.88901° |
Longitude | -121.47664° |
Altitude | 506.052 km |
Speed | 7.617 km/s |
Apparent Right ascension | 09h 29m 19s |
Apparent Declination | -9° 54' 20" |
Sunlit | Object is in full shadow |
Visualization observer readout
Local Sidereal Time | 16:05:24 |
Azimuth | 268.069° W |
Elevation | -13.231° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 517.3 km |
Perigee altitude | 499.006 km |
Semi-major axis | 6,886.29 km |
Eccentricity | 0.0013283 |
Inclination | 52.979° |
RAAN | 45.0544° |
Arg. of periapsis | 70.4407° |
True anomaly | 289.65871° |
Mean anomaly | 289.802° |
Eccentric anomaly | 289.73036° |
Mean motion | 3.79809 °/min |
BSTAR | 0.00035164 |
Orbital period | 94.78 mins |
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Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
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. |
---|---|---|---|---|---|---|---|
6 mins | 2025-02-13 01:44:28.333Z | 189.894° SSW | 2025-02-13 01:47:28.333Z | 118.618° SE | 27.649° | 2025-02-13 01:50:28.333Z | 68.212° E |
5 mins | 2025-02-13 03:23:28.333Z | 273.757° WNW | 2025-02-13 03:25:28.333Z | 321.613° NNW | 29.252° | 2025-02-13 03:28:28.333Z | 30.775° NE |
5 mins | 2025-02-13 08:22:28.333Z | 333.826° NNW | 2025-02-13 08:24:28.333Z | 19.719° NNE | 29.701° | 2025-02-13 08:27:28.333Z | 92.719° ESE |
5 mins | 2025-02-13 10:01:28.333Z | 275.766° WNW | 2025-02-13 10:03:28.333Z | 224.469° SW | 27.464° | 2025-02-13 10:06:28.333Z | 166.97° S |
Authenticating...
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