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: 22 hours ago
TLE from 22 hours ago
0 SPACEMOBILE-012
1 A0241U 26179B 26263.02592382 .00001227 00000-0 84950-4 0 9994
2 A0241 52.9948 120.4139 0007529 111.3755 248.8040 15.13299819 6923Epoch: 2026-09-20T00:37Z
TLE epoch observation values (Epoch: 2026-09-20T00:37:19.818Z)
Latitude
-0.00002°
Longitude
112.15529°
Altitude
528.903 km
Speed
7.599 km/s
True Right ascension
08h 01m 39s
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
15:21:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.625 km
Perigee altitude
521.228 km
Semi-major axis
6,904.563 km
Eccentricity
0.00075
Inclination
52.9948°
RAAN
120.4139°
Arg. of periapsis
111.3755°
True anomaly
248.72359°
Mean anomaly
248.804°
Eccentric anomaly
248.76379°
Mean motion
3.78302 °/min
Orbital period
95.16 mins
BSTAR
0.00008495
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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 | 2026-09-20 23:17:04.590Z | 326.683° NNW | 2026-09-20 23:20:04.590Z | 28.942° NE | 37.205° | 2026-09-20 23:23:04.590Z | 95.421° ESE |
| 5 mins | 2026-09-21 00:57:04.590Z | 277.238° WNW | 2026-09-21 00:59:04.590Z | 230.019° WSW | 31.369° | 2026-09-21 01:02:04.590Z | 169.623° S |
| 6 mins | 2026-09-21 16:25:04.590Z | 195.824° SSW | 2026-09-21 16:27:04.590Z | 154.051° SSE | 39.273° | 2026-09-21 16:31:04.590Z | 64.203° ENE |
| 5 mins | 2026-09-21 18:05:04.590Z | 289.173° WNW | 2026-09-21 18:07:04.590Z | 343.064° N | 30.455° | 2026-09-21 18:10:04.590Z | 33.506° NE |
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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