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 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: 11 hours ago
TLE from 11 hours ago
0 SPACEMOBILE-009
1 69590U 26139B 26278.53781999 .00000641 00000-0 52808-4 0 9994
2 69590 52.9932 121.5624 0002653 311.8743 48.2022 15.12923866 16687Epoch: 2026-10-05T12:54Z
TLE epoch observation values (Epoch: 2026-10-05T12:54:27.647Z)
Latitude
0.00004°
Longitude
-86.26804°
Altitude
526.943 km
Speed
7.601 km/s
True Right ascension
08h 06m 14s
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
17:32:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.402 km
Perigee altitude
525.738 km
Semi-major axis
6,905.707 km
Eccentricity
0.00027
Inclination
52.9932°
RAAN
121.5624°
Arg. of periapsis
311.8743°
True anomaly
48.22487°
Mean anomaly
48.2022°
Eccentric anomaly
48.21353°
Mean motion
3.78208 °/min
Orbital period
95.19 mins
BSTAR
0.000052808
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-06 00:34:02.915Z | 272.899° WNW | 2026-10-06 00:36:02.915Z | 238.561° WSW | 20.248° | 2026-10-06 00:39:02.915Z | 186.244° SSW |
| 6 mins | 2026-10-06 16:03:02.915Z | 212.92° SW | 2026-10-06 16:05:02.915Z | 141.245° SSE | 67.018° | 2026-10-06 16:09:02.915Z | 54.979° ENE |
| 4 mins | 2026-10-06 17:43:02.915Z | 303.822° NW | 2026-10-06 17:44:02.915Z | 325.089° NNW | 23.633° | 2026-10-06 17:47:02.915Z | 23.592° NE |
| 6 mins | 2026-10-06 22:42:02.915Z | 318.468° NNW | 2026-10-06 22:45:02.915Z | 55.6° ENE | 62.81° | 2026-10-06 22:48:02.915Z | 117.447° 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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