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 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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100240 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, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 SPACEMOBILE-013
1 A0240U 26179A 26263.88967291 .00000887 00000-0 66401-4 0 9994
2 A0240 52.9954 116.5479 0007350 107.5368 252.6427 15.13135241 7056Epoch: 2026-09-20T21:21Z
TLE epoch observation values (Epoch: 2026-09-20T21:21:07.739Z)
Latitude
0°
Longitude
156.48828°
Altitude
529.038 km
Speed
7.599 km/s
True Right ascension
07h 46m 11s
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
03:10:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
532.002 km
Perigee altitude
521.851 km
Semi-major axis
6,905.064 km
Eccentricity
0.00074
Inclination
52.9954°
RAAN
116.5479°
Arg. of periapsis
107.5368°
True anomaly
252.56233°
Mean anomaly
252.6427°
Eccentric anomaly
252.60251°
Mean motion
3.78261 °/min
Orbital period
95.17 mins
BSTAR
0.000066401
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-21 16:32:21.291Z | 206.187° SW | 2026-09-21 16:35:21.291Z | 138.721° SSE | 48.685° | 2026-09-21 16:38:21.291Z | 64.319° ENE |
| 5 mins | 2026-09-21 18:12:21.291Z | 283.23° WNW | 2026-09-21 18:14:21.291Z | 324.381° NNW | 27.94° | 2026-09-21 18:17:21.291Z | 26.516° NE |
| 6 mins | 2026-09-21 23:12:21.291Z | 325.003° NNW | 2026-09-21 23:15:21.291Z | 52.154° ENE | 47.224° | 2026-09-21 23:18:21.291Z | 108.216° ESE |
| 4 mins | 2026-09-22 00:52:21.291Z | 262.593° W | 2026-09-22 00:53:21.291Z | 242.504° WSW | 21.984° | 2026-09-22 00:56:21.291Z | 184.899° SSW |
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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