SPACEMOBILE-011, 100242
Orbit data source: Space-Track
SPACEMOBILE-011, 100242 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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100242 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, 5.0 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SPACEMOBILE-011
1 A0242U 26179C 26263.02342991 .00000090 00000-0 21835-4 0 9994
2 A0242 52.9958 120.4034 0007021 114.7125 245.4598 15.13339449 6929Epoch: 2026-09-20T00:33Z
TLE epoch observation values (Epoch: 2026-09-20T00:33:44.344Z)
Latitude
0.00001°
Longitude
113.04508°
Altitude
528.916 km
Speed
7.599 km/s
True Right ascension
08h 01m 36s
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
22:52:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.153 km
Perigee altitude
521.458 km
Semi-major axis
6,904.442 km
Eccentricity
0.0007
Inclination
52.9958°
RAAN
120.4034°
Arg. of periapsis
114.7125°
True anomaly
245.38664°
Mean anomaly
245.4598°
Eccentric anomaly
245.42322°
Mean motion
3.78312 °/min
Orbital period
95.16 mins
BSTAR
0.000021835
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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-011 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-21 16:20:29.277Z | 199.293° SSW | 2026-09-21 16:23:29.277Z | 144.577° SSE | 37.548° | 2026-09-21 16:27:29.277Z | 64.5° ENE |
| 6 mins | 2026-09-21 18:00:29.277Z | 275.668° WNW | 2026-09-21 18:02:29.277Z | 317.909° NNW | 32.061° | 2026-09-21 18:06:29.277Z | 35.616° NE |
| 6 mins | 2026-09-21 23:00:29.277Z | 327.956° NNW | 2026-09-21 23:03:29.277Z | 42.58° NE | 39.721° | 2026-09-21 23:06:29.277Z | 100.669° ESE |
| 5 mins | 2026-09-22 00:40:29.277Z | 269.594° W | 2026-09-22 00:42:29.277Z | 220.216° SW | 28° | 2026-09-22 00:45:29.277Z | 169.95° 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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