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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69589 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: 12 hours ago
TLE from 12 hours ago
0 SPACEMOBILE-008
1 69589U 26139A 26214.38663074 .00001353 00000-0 92961-4 0 9993
2 69589 52.9954 52.8129 0005349 99.6449 260.5146 15.12859078 6974Epoch: 2026-08-02T09:16Z
TLE epoch observation values (Epoch: 2026-08-02T09:16:44.895Z)
Latitude
-0.00009°
Longitude
-37.35906°
Altitude
528.972 km
Speed
7.599 km/s
True Right ascension
03h 31m 15s
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
10:49:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.461 km
Perigee altitude
524.073 km
Semi-major axis
6,905.904 km
Eccentricity
0.00053
Inclination
52.9954°
RAAN
52.8129°
Arg. of periapsis
99.6449°
True anomaly
260.45415°
Mean anomaly
260.5146°
Eccentric anomaly
260.48437°
Mean motion
3.78192 °/min
Orbital period
95.19 mins
BSTAR
0.000092961
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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-008 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 | 2026-08-02 22:26:29.309Z | 318.959° NNW | 2026-08-02 22:30:29.309Z | 62.82° ENE | 36.721° | 2026-08-02 22:33:29.309Z | 111.159° ESE |
| 4 mins | 2026-08-03 00:07:29.309Z | 258.705° W | 2026-08-03 00:08:29.309Z | 238.599° WSW | 19.532° | 2026-08-03 00:11:29.309Z | 184.989° SSW |
| 6 mins | 2026-08-03 15:35:29.309Z | 210.594° SW | 2026-08-03 15:37:29.309Z | 149.422° SSE | 41.469° | 2026-08-03 15:41:29.309Z | 56.22° ENE |
| 4 mins | 2026-08-03 17:15:29.309Z | 301.206° NW | 2026-08-03 17:16:29.309Z | 322.558° NNW | 22.089° | 2026-08-03 17:19:29.309Z | 23.26° NE |
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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