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 spacecraft
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
Unknown shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 SPACEMOBILE-010
1 69591U 26139C 26202.43522734 .00001174 00000-0 83597-4 0 9992
2 69591 52.9950 107.1407 0005562 60.2042 299.9501 15.12546197 5173Epoch: 2026-07-21T10:26Z
TLE epoch observation values (Epoch: 2026-07-21T10:26:43.642Z)
Latitude
-0.00004°
Longitude
11.25387°
Altitude
527.397 km
Speed
7.602 km/s
True Right ascension
07h 08m 33s
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
18:38:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
532.561 km
Perigee altitude
524.878 km
Semi-major axis
6,906.856 km
Eccentricity
0.00056
Inclination
52.995°
RAAN
107.1407°
Arg. of periapsis
60.2042°
True anomaly
299.89486°
Mean anomaly
299.9501°
Eccentric anomaly
299.92248°
Mean motion
3.78114 °/min
Orbital period
95.21 mins
BSTAR
0.000083597
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-07-22 19:54:43.155Z | 215.949° SW | 2026-07-22 19:58:43.155Z | 100.021° ESE | 39.562° | 2026-07-22 20:01:43.155Z | 57.49° ENE |
| 5 mins | 2026-07-22 21:35:43.155Z | 294.214° NW | 2026-07-22 21:37:43.155Z | 337.55° N | 22.73° | 2026-07-22 21:40:43.155Z | 29.579° NE |
| 4 mins | 2026-07-23 00:56:43.155Z | 349.453° N | 2026-07-23 00:58:43.155Z | 25.648° NE | 16.139° | 2026-07-23 01:00:43.155Z | 57.033° ENE |
| 6 mins | 2026-07-23 02:35:43.155Z | 322.208° NNW | 2026-07-23 02:37:43.155Z | 10.702° NNE | 40.246° | 2026-07-23 02:41:43.155Z | 117.09° 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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