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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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Identifier
100242, 2026-179C
Orbit
LEO
Country
Flag of USUS
Related 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)
2026-08-05 (2 months ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL + 2 PAN + PLATE, 5.0 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last 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  6929
Epoch: 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
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
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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