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SPACEMOBILE-008, 69589

Orbit data source: Space-Track

SPACEMOBILE-008, 69589 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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Identifier
69589, 2026-139A
Orbit
LEO
Country
Flag of USUS
Related 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)
2026-06-17 (4 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 2 Pan + 1 Plate, 14.5 m
Radar Cross Section
24.992 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 SPACEMOBILE-008
1 69589U 26139A   26278.53017106  .00000766  00000-0  59701-4 0  9991
2 69589  52.9939 121.5282 0002507 320.2938  39.7869 15.13028844 16687
Epoch: 2026-10-05T12:43Z
TLE epoch observation values (Epoch: 2026-10-05T12:43:26.779Z)
Latitude
-0.00005°
Longitude
-83.54116°
Altitude
526.515 km
Speed
7.602 km/s
True Right ascension
08h 06m 06s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
16:27:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.982 km
Perigee altitude
525.519 km
Semi-major axis
6,905.388 km
Eccentricity
0.00025
Inclination
52.9939°
RAAN
121.5282°
Arg. of periapsis
320.2938°
True anomaly
39.80529°
Mean anomaly
39.7869°
Eccentric anomaly
39.79609°
Mean motion
3.78234 °/min
Orbital period
95.18 mins
BSTAR
0.000059701
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Other satellites on launch #139 in the year 2026 (2026-06-17 UTC)

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