SPACEMOBILE-009, 69590
Orbit data source: Space-Track
SPACEMOBILE-009, 69590 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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69590 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, 5.0 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 SPACEMOBILE-009
1 69590U 26139B 26202.43143916 .00001219 00000-0 85768-4 0 9994
2 69590 52.9944 107.1141 0005567 67.5981 292.5599 15.12709273 5168Epoch: 2026-07-21T10:21Z
TLE epoch observation values (Epoch: 2026-07-21T10:21:16.343Z)
Latitude
-0.00004°
Longitude
12.59475°
Altitude
527.344 km
Speed
7.601 km/s
True Right ascension
07h 08m 27s
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
17:46:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
532.068 km
Perigee altitude
524.378 km
Semi-major axis
6,906.36 km
Eccentricity
0.00056
Inclination
52.9944°
RAAN
107.1141°
Arg. of periapsis
67.5981°
True anomaly
292.50097°
Mean anomaly
292.5599°
Eccentric anomaly
292.53044°
Mean motion
3.78155 °/min
Orbital period
95.2 mins
BSTAR
0.000085768
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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-009 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 | 2026-07-22 19:49:19.138Z | 209.917° SW | 2026-07-22 19:52:19.138Z | 138.422° SSE | 39.016° | 2026-07-22 19:55:19.138Z | 61.924° ENE |
| 5 mins | 2026-07-22 21:29:19.138Z | 285.141° WNW | 2026-07-22 21:31:19.138Z | 324.53° NNW | 23.782° | 2026-07-22 21:34:19.138Z | 25.638° NE |
| 6 mins | 2026-07-23 02:29:19.138Z | 321.935° NNW | 2026-07-23 02:32:19.138Z | 50.897° ENE | 38.727° | 2026-07-23 02:35:19.138Z | 111.688° ESE |
| 4 mins | 2026-07-23 04:09:19.138Z | 262.096° W | 2026-07-23 04:11:19.138Z | 222.375° SW | 18.607° | 2026-07-23 04:13:19.138Z | 189.134° 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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