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: 14 hours ago
TLE from 14 hours ago
0 SPACEMOBILE-011
1 A0242U 26179C 26251.20189279 .00000686 00000-0 54924-4 0 9995
2 A0242 52.9960 174.1183 0007132 84.8111 275.3694 15.13332295 5131Epoch: 2026-09-08T04:50Z
TLE epoch observation values (Epoch: 2026-09-08T04:50:43.537Z)
Latitude
-0°
Longitude
114.1652°
Altitude
526.465 km
Speed
7.601 km/s
True Right ascension
11h 36m 28s
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
11:08:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.251 km
Perigee altitude
521.403 km
Semi-major axis
6,904.464 km
Eccentricity
0.00071
Inclination
52.996°
RAAN
174.1183°
Arg. of periapsis
84.8111°
True anomaly
275.28803°
Mean anomaly
275.3694°
Eccentric anomaly
275.32871°
Mean motion
3.7831 °/min
Orbital period
95.16 mins
BSTAR
0.000054924
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-08 20:50:43.454Z | 188.77° SSW | 2026-09-08 20:53:43.454Z | 133.377° SE | 28.907° | 2026-09-08 20:56:43.454Z | 74.713° E |
| 5 mins | 2026-09-08 22:30:43.454Z | 271.486° WNW | 2026-09-08 22:32:43.454Z | 326.811° NNW | 39.658° | 2026-09-08 22:35:43.454Z | 33.576° NE |
| 6 mins | 2026-09-09 03:30:43.454Z | 334.816° NNW | 2026-09-09 03:32:43.454Z | 16.599° NNE | 32.244° | 2026-09-09 03:36:43.454Z | 95.591° ESE |
| 6 mins | 2026-09-09 05:09:43.454Z | 286.18° WNW | 2026-09-09 05:11:43.454Z | 244.899° WSW | 35.862° | 2026-09-09 05:15:43.454Z | 159.895° 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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