SPACEMOBILE-010, 69591
Orbit data source: Space-Track
SPACEMOBILE-010, 69591 is a payload satellite owned by AST & Science (US) in LEO that was launched on Wed, 17 Jun 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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69591 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
5,850 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: 1 day ago
TLE from 1 day ago
0 SPACEMOBILE-010
1 69591U 26139C 26277.95453573 .00000661 00000-0 54124-4 0 9999
2 69591 52.9936 124.3373 0002629 293.9339 66.1376 15.12782550 16604Epoch: 2026-10-04T22:54Z
TLE epoch observation values (Epoch: 2026-10-04T22:54:31.887Z)
Latitude
-0.00004°
Longitude
127.06404°
Altitude
527.86 km
Speed
7.601 km/s
True Right ascension
08h 17m 20s
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
17:32:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.816 km
Perigee altitude
526.184 km
Semi-major axis
6,906.137 km
Eccentricity
0.00026
Inclination
52.9936°
RAAN
124.3373°
Arg. of periapsis
293.9339°
True anomaly
66.16515°
Mean anomaly
66.1376°
Eccentric anomaly
66.15138°
Mean motion
3.78173 °/min
Orbital period
95.19 mins
BSTAR
0.000054124
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Other satellites on launch #139 in the year 2026 (2026-06-17 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-010 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 | 2026-10-06 00:51:02.607Z | 267.65° W | 2026-10-06 00:53:02.607Z | 237.482° WSW | 14.49° | 2026-10-06 00:55:02.607Z | 205.481° SW |
| 6 mins | 2026-10-06 16:20:02.607Z | 231.133° WSW | 2026-10-06 16:22:02.607Z | 254.639° W | 83.552° | 2026-10-06 16:26:02.607Z | 49.763° ENE |
| 4 mins | 2026-10-06 18:00:02.607Z | 306.099° NW | 2026-10-06 18:02:02.607Z | 345.29° N | 20.225° | 2026-10-06 18:04:02.607Z | 19.878° NNE |
| 4 mins | 2026-10-06 21:21:02.607Z | 353.61° N | 2026-10-06 21:22:02.607Z | 12.879° NNE | 20.166° | 2026-10-06 21:25:02.607Z | 66.228° ENE |
| 6 mins | 2026-10-06 22:59:02.607Z | 310.586° NW | 2026-10-06 23:02:02.607Z | 75.933° E | 87.006° | 2026-10-06 23:05:02.607Z | 129.609° SE |
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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