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 26251.20774972 .00001649 00000-0 10895-3 0 9991
2 A0240 52.9959 174.1527 0007312 75.8148 284.3656 15.13099502 5138Epoch: 2026-09-08T04:59Z
TLE epoch observation values (Epoch: 2026-09-08T04:59:09.575Z)
Latitude
0.00003°
Longitude
112.08536°
Altitude
526.381 km
Speed
7.602 km/s
True Right ascension
11h 36m 36s
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
10:07:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
532.084 km
Perigee altitude
521.986 km
Semi-major axis
6,905.172 km
Eccentricity
0.00073
Inclination
52.9959°
RAAN
174.1527°
Arg. of periapsis
75.8148°
True anomaly
284.28441°
Mean anomaly
284.3656°
Eccentric anomaly
284.32501°
Mean motion
3.78252 °/min
Orbital period
95.17 mins
BSTAR
0.00010895
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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 | 2026-09-08 21:00:00.410Z | 191.174° SSW | 2026-09-08 21:03:00.410Z | 120.895° SE | 33.989° | 2026-09-08 21:06:00.410Z | 68.325° E |
| 5 mins | 2026-09-08 22:40:00.410Z | 282.093° WNW | 2026-09-08 22:42:00.410Z | 339.226° N | 34.371° | 2026-09-08 22:45:00.410Z | 33.979° NE |
| 5 mins | 2026-09-09 03:40:00.410Z | 335.609° NNW | 2026-09-09 03:42:00.410Z | 25.65° NE | 37.42° | 2026-09-09 03:45:00.410Z | 94.955° ESE |
| 5 mins | 2026-09-09 05:19:00.410Z | 278.327° WNW | 2026-09-09 05:21:00.410Z | 233.151° WSW | 31.109° | 2026-09-09 05:24:00.410Z | 170.832° 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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