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 launched 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 spacecraft
Bus & Motor
BB BLOCK-2, EP
Mass
6,740 kg wet, 5,830 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
CYL + 2 PAN + PLATE, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 SPACEMOBILE-012
1 A0241U 26179B 26251.20396745 .00001657 00000-0 10892-3 0 9996
2 A0241 52.9953 174.1264 0007477 81.2305 278.9533 15.13267160 5139Epoch: 2026-09-08T04:53Z
TLE epoch observation values (Epoch: 2026-09-08T04:53:42.787Z)
Latitude
-0.00001°
Longitude
113.42437°
Altitude
526.32 km
Speed
7.602 km/s
True Right ascension
11h 36m 30s
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
10:42:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.688 km
Perigee altitude
521.363 km
Semi-major axis
6,904.662 km
Eccentricity
0.00075
Inclination
52.9953°
RAAN
174.1264°
Arg. of periapsis
81.2305°
True anomaly
278.86865°
Mean anomaly
278.9533°
Eccentric anomaly
278.91098°
Mean motion
3.78294 °/min
Orbital period
95.16 mins
BSTAR
0.00010892
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-08 20:53:53.673Z | 190.492° SSW | 2026-09-08 20:56:53.673Z | 132.778° SE | 30.791° | 2026-09-08 20:59:53.673Z | 73.226° E |
| 5 mins | 2026-09-08 22:33:53.673Z | 273.7° WNW | 2026-09-08 22:35:53.673Z | 327.557° NNW | 37.813° | 2026-09-08 22:38:53.673Z | 32.865° NE |
| 6 mins | 2026-09-09 03:33:53.673Z | 333.97° NNW | 2026-09-09 03:35:53.673Z | 16.146° NNE | 33.587° | 2026-09-09 03:39:53.673Z | 97.148° ESE |
| 6 mins | 2026-09-09 05:12:53.673Z | 284.559° WNW | 2026-09-09 05:14:53.673Z | 243.625° WSW | 33.815° | 2026-09-09 05:18:53.673Z | 161.843° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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