SPACEMOBILE-006, 67232
Orbit data source: Space-Track
SPACEMOBILE-006, 67232 is a payload satellite owned by AST & Science (US) in LEO that was launched on Wed, 24 Dec 2025 UTC via a LVM3 launch vehicle from the Sirharikota (SRI). 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
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: 14 hours ago
TLE from 14 hours ago
0 SPACEMOBILE-006
1 67232U 25309A 26253.39594899 .00001476 00000-0 85134-4 0 9996
2 67232 52.9947 301.2448 0011508 41.2332 318.9529 15.18870356 39542Epoch: 2026-09-10T09:30Z
TLE epoch observation values (Epoch: 2026-09-10T09:30:09.992Z)
Latitude
-0.00002°
Longitude
169.26889°
Altitude
504.158 km
Speed
7.617 km/s
True Right ascension
20h 04m 58s
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
15:33:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
517.462 km
Perigee altitude
501.609 km
Semi-major axis
6,887.672 km
Eccentricity
0.00115
Inclination
52.9947°
RAAN
301.2448°
Arg. of periapsis
41.2332°
True anomaly
318.86621°
Mean anomaly
318.9529°
Eccentric anomaly
318.90956°
Mean motion
3.79695 °/min
Orbital period
94.81 mins
BSTAR
0.000085134
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Other satellites on launch #309 in the year 2025 (2025-12-24 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-006 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 | 2026-09-11 06:14:31.270Z | 243.413° WSW | 2026-09-11 06:16:31.270Z | 335.38° NNW | 70.05° | 2026-09-11 06:19:31.270Z | 44.973° NE |
| 5 mins | 2026-09-11 11:13:31.270Z | 344.358° N | 2026-09-11 11:15:31.270Z | 23.834° NE | 21.448° | 2026-09-11 11:18:31.270Z | 74.814° E |
| 5 mins | 2026-09-11 12:52:31.270Z | 304.223° NW | 2026-09-11 12:54:31.270Z | 227.322° WSW | 77.702° | 2026-09-11 12:57:31.270Z | 136.855° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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