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 26259.39111622 .00000322 00000-0 34721-4 0 9990
2 A0242 52.9961 136.9089 0007098 104.8233 255.3545 15.13340056 6376Epoch: 2026-09-16T09:23Z
TLE epoch observation values (Epoch: 2026-09-16T09:23:12.441Z)
Latitude
-0.00001°
Longitude
0.76367°
Altitude
528.141 km
Speed
7.599 km/s
True Right ascension
09h 07m 38s
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
02:03:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.204 km
Perigee altitude
521.403 km
Semi-major axis
6,904.441 km
Eccentricity
0.00071
Inclination
52.9961°
RAAN
136.9089°
Arg. of periapsis
104.8233°
True anomaly
255.27582°
Mean anomaly
255.3545°
Eccentric anomaly
255.31516°
Mean motion
3.78312 °/min
Orbital period
95.16 mins
BSTAR
0.000034721
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-17 17:14:07.707Z | 169.5° S | 2026-09-17 17:16:07.707Z | 137.373° SSE | 18.507° | 2026-09-17 17:19:07.707Z | 85.482° E |
| 6 mins | 2026-09-17 18:53:07.707Z | 252.429° W | 2026-09-17 18:55:07.707Z | 309.767° NW | 56.549° | 2026-09-17 18:59:07.707Z | 43.371° NE |
| 4 mins | 2026-09-17 23:54:07.707Z | 351.582° N | 2026-09-17 23:55:07.707Z | 13.129° NNE | 24.568° | 2026-09-17 23:58:07.707Z | 74.875° E |
| 6 mins | 2026-09-18 01:32:07.707Z | 299.375° NW | 2026-09-18 01:35:07.707Z | 206.926° SW | 58.246° | 2026-09-18 01:38:07.707Z | 146.272° 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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