SPACEMOBILE-012, 100241
Orbit data source: Space-Track
SPACEMOBILE-012, 100241 is a payload satellite owned by AST & Science (US) in LEO that was launched on Wed, 05 Aug 2026 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft 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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100241 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
AST & Science
Mission
Operational Commercial Communications
Bus & Motor
BB BLOCK-2, EP
Mass
6,740 kg wet, 5,830 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan + 1 Plate, 14.5 m
Radar Cross Section
24.992 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SPACEMOBILE-012
1 A0241U 26179B 26316.98052156 .00002458 00000-0 15245-3 0 9995
2 A0241 52.9945 235.2326 0004454 287.7775 72.2730 15.13486381 15092Epoch: 2026-11-12T23:31Z
TLE epoch observation values (Epoch: 2026-11-12T23:31:57.062Z)
Latitude
-0.00005°
Longitude
-169.86142°
Altitude
525.518 km
Speed
7.602 km/s
True Right ascension
15h 40m 55s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
20:20:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.934 km
Perigee altitude
522.784 km
Semi-major axis
6,903.996 km
Eccentricity
0.00045
Inclination
52.9945°
RAAN
235.2326°
Arg. of periapsis
287.7775°
True anomaly
72.32162°
Mean anomaly
72.273°
Eccentric anomaly
72.29731°
Mean motion
3.78349 °/min
Orbital period
95.15 mins
BSTAR
0.00015245
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Other satellites on launch #179 in the year 2026 (2026-08-05 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SPACEMOBILE-012 Visibility forecast
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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 | 2026-11-14 02:57:02.135Z | 345.54° N | 2026-11-14 02:59:02.135Z | 32.144° NE | 27.542° | 2026-11-14 03:02:02.135Z | 84.943° E |
| 5 mins | 2026-11-14 04:36:02.135Z | 289.948° WNW | 2026-11-14 04:38:02.135Z | 227.216° WSW | 51.624° | 2026-11-14 04:41:02.135Z | 152.555° SSE |
| 5 mins | 2026-11-14 20:04:02.135Z | 176.912° S | 2026-11-14 20:06:02.135Z | 138.653° SSE | 25.378° | 2026-11-14 20:09:02.135Z | 79.418° E |
| 6 mins | 2026-11-14 21:43:02.135Z | 264.706° W | 2026-11-14 21:45:02.135Z | 317.022° NNW | 43.716° | 2026-11-14 21:49:02.135Z | 39.856° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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