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: 11 hours ago
TLE from 11 hours ago
0 SPACEMOBILE-012
1 A0241U 26179B 26259.92185956 .00001538 00000-0 10225-3 0 9991
2 A0241 52.9954 134.5174 0007506 103.3448 256.8380 15.13292443 6450Epoch: 2026-09-16T22:07Z
TLE epoch observation values (Epoch: 2026-09-16T22:07:28.665Z)
Latitude
-0.00009°
Longitude
166.78139°
Altitude
528.227 km
Speed
7.599 km/s
True Right ascension
08h 58m 04s
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
02:01:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.631 km
Perigee altitude
521.266 km
Semi-major axis
6,904.585 km
Eccentricity
0.00075
Inclination
52.9954°
RAAN
134.5174°
Arg. of periapsis
103.3448°
True anomaly
256.75427°
Mean anomaly
256.838°
Eccentric anomaly
256.79613°
Mean motion
3.783 °/min
Orbital period
95.16 mins
BSTAR
0.00010225
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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 | 2026-09-17 17:18:05.461Z | 167.183° S | 2026-09-17 17:20:05.461Z | 130.969° SE | 20.25° | 2026-09-17 17:23:05.461Z | 80.823° E |
| 6 mins | 2026-09-17 18:56:05.461Z | 250.507° W | 2026-09-17 18:59:05.461Z | 332.235° NNW | 53.423° | 2026-09-17 19:02:05.461Z | 39.591° NE |
| 5 mins | 2026-09-17 23:57:05.461Z | 340.046° N | 2026-09-17 23:59:05.461Z | 20.71° NNE | 26.175° | 2026-09-18 00:02:05.461Z | 79.732° E |
| 6 mins | 2026-09-18 01:36:05.461Z | 295.613° NW | 2026-09-18 01:38:05.461Z | 254.122° W | 50.788° | 2026-09-18 01:42:05.461Z | 147.746° SSE |
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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