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 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-008
1 69589U 26139A 26202.42904412 .00000319 00000-0 34924-4 0 9995
2 69589 52.9953 107.1053 0005298 71.2526 288.9040 15.12809290 5166Epoch: 2026-07-21T10:17Z
TLE epoch observation values (Epoch: 2026-07-21T10:17:49.411Z)
Latitude
-0.00001°
Longitude
13.45055°
Altitude
527.329 km
Speed
7.601 km/s
True Right ascension
07h 08m 25s
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
17:38:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.577 km
Perigee altitude
524.26 km
Semi-major axis
6,906.055 km
Eccentricity
0.00053
Inclination
52.9953°
RAAN
107.1053°
Arg. of periapsis
71.2526°
True anomaly
288.84655°
Mean anomaly
288.904°
Eccentric anomaly
288.87528°
Mean motion
3.7818 °/min
Orbital period
95.19 mins
BSTAR
0.000034924
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-22 19:45:38.538Z | 206.911° SW | 2026-07-22 19:48:38.538Z | 135.401° SSE | 37.443° | 2026-07-22 19:51:38.538Z | 63.422° ENE |
| 5 mins | 2026-07-22 21:25:38.538Z | 284.279° WNW | 2026-07-22 21:27:38.538Z | 325.658° NNW | 24.753° | 2026-07-22 21:30:38.538Z | 26.894° NE |
| 6 mins | 2026-07-23 02:25:38.538Z | 323.869° NNW | 2026-07-23 02:28:38.538Z | 53.154° ENE | 37.165° | 2026-07-23 02:31:38.538Z | 109.66° ESE |
| 4 mins | 2026-07-23 04:05:38.538Z | 262.123° W | 2026-07-23 04:07:38.538Z | 220.168° SW | 19.756° | 2026-07-23 04:09:38.538Z | 186.388° 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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