SPACEMOBILE-013, 100240
Orbit data source: Space-Track
SPACEMOBILE-013, 100240 is a payload satellite owned by AST & Science (US) in LEO that was launched on Wed, 05 Aug 2026 UTC via an FALCON 9 launch vehicle 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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100240 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
AST & Science
Mission
Operational Commercial Communications
Bus & Motor
BB BLOCK-2, EP
Mass
6,740 kg wet, 5,830 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan + 1 Plate, 14.5 m
Radar Cross Section
24.992 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 SPACEMOBILE-013
1 A0240U 26179A 26317.19005844 .00003092 00000-0 18834-3 0 9992
2 A0240 52.9952 234.4082 0004303 281.0425 79.0082 15.13302140 15120Epoch: 2026-11-13T04:33Z
TLE epoch observation values (Epoch: 2026-11-13T04:33:41.049Z)
Latitude
-0.00002°
Longitude
113.67439°
Altitude
526.448 km
Speed
7.601 km/s
True Right ascension
15h 37m 37s
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
20:20:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.39 km
Perigee altitude
523.448 km
Semi-major axis
6,904.556 km
Eccentricity
0.00043
Inclination
52.9952°
RAAN
234.4082°
Arg. of periapsis
281.0425°
True anomaly
79.05661°
Mean anomaly
79.0082°
Eccentric anomaly
79.0324°
Mean motion
3.78303 °/min
Orbital period
95.16 mins
BSTAR
0.00018834
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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-013 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-13 23:54:02.167Z | 320.271° NNW | 2026-11-13 23:56:02.167Z | 352.467° N | 14.518° | 2026-11-13 23:58:02.167Z | 22.531° NE |
| 5 mins | 2026-11-14 03:14:02.167Z | 336.644° NNW | 2026-11-14 03:16:02.167Z | 22.814° NE | 34.153° | 2026-11-14 03:19:02.167Z | 90.338° ESE |
| 5 mins | 2026-11-14 04:53:02.167Z | 282.957° WNW | 2026-11-14 04:55:02.167Z | 237.48° WSW | 35.599° | 2026-11-14 04:58:02.167Z | 167.247° S |
| 6 mins | 2026-11-14 20:21:02.167Z | 192.482° SSW | 2026-11-14 20:24:02.167Z | 120.044° SE | 35.621° | 2026-11-14 20:27:02.167Z | 67.504° E |
| 5 mins | 2026-11-14 22:01:02.167Z | 283.512° WNW | 2026-11-14 22:03:02.167Z | 339.4° N | 33.726° | 2026-11-14 22:06:02.167Z | 33.605° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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