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: 11 hours ago
TLE from 11 hours ago
0 SPACEMOBILE-013
1 A0240U 26179A 26259.92660705 .00001708 00000-0 11217-3 0 9991
2 A0240 52.9958 134.5501 0007387 97.7042 262.4788 15.13126397 6459Epoch: 2026-09-16T22:14Z
TLE epoch observation values (Epoch: 2026-09-16T22:14:18.849Z)
Latitude
-0.00002°
Longitude
165.10036°
Altitude
528.219 km
Speed
7.6 km/s
True Right ascension
08h 58m 12s
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
01:59:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
532.054 km
Perigee altitude
521.853 km
Semi-major axis
6,905.09 km
Eccentricity
0.00074
Inclination
52.9958°
RAAN
134.5501°
Arg. of periapsis
97.7042°
True anomaly
262.39489°
Mean anomaly
262.4788°
Eccentric anomaly
262.43684°
Mean motion
3.78259 °/min
Orbital period
95.17 mins
BSTAR
0.00011217
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-17 17:25:03.664Z | 174.149° S | 2026-09-17 17:27:03.664Z | 137.54° SSE | 23.075° | 2026-09-17 17:30:03.664Z | 80.974° E |
| 6 mins | 2026-09-17 19:04:03.664Z | 261.407° W | 2026-09-17 19:06:03.664Z | 316.06° NNW | 46.95° | 2026-09-17 19:10:03.664Z | 40.904° NE |
| 5 mins | 2026-09-18 00:05:03.664Z | 348.925° N | 2026-09-18 00:07:03.664Z | 39.914° NE | 28.087° | 2026-09-18 00:10:03.664Z | 88.9° E |
| 6 mins | 2026-09-18 01:43:03.664Z | 293.942° NW | 2026-09-18 01:46:03.664Z | 213.762° SW | 46.345° | 2026-09-18 01:49:03.664Z | 154.155° SSE |
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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