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: 1 day ago
TLE from 1 day ago
0 SPACEMOBILE-006
1 67232U 25309A 26259.05482892 .00002488 00000-0 13289-3 0 9999
2 67232 52.9950 275.3101 0011997 56.8331 303.3812 15.18896980 40407Epoch: 2026-09-16T01:18Z
TLE epoch observation values (Epoch: 2026-09-16T01:18:57.218Z)
Latitude
-0.00001°
Longitude
-99.44024°
Altitude
505.511 km
Speed
7.615 km/s
True Right ascension
18h 21m 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
02:00:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
517.718 km
Perigee altitude
501.192 km
Semi-major axis
6,887.592 km
Eccentricity
0.0012
Inclination
52.995°
RAAN
275.3101°
Arg. of periapsis
56.8331°
True anomaly
303.26631°
Mean anomaly
303.3812°
Eccentric anomaly
303.32376°
Mean motion
3.79701 °/min
Orbital period
94.81 mins
BSTAR
0.00013289
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-17 09:21:27.423Z | 333.039° NNW | 2026-09-17 09:24:27.423Z | 33.994° NE | 26.708° | 2026-09-17 09:27:27.423Z | 86.115° E |
| 6 mins | 2026-09-17 11:00:27.423Z | 294.423° NW | 2026-09-17 11:03:27.423Z | 202.2° SSW | 47.228° | 2026-09-17 11:06:27.423Z | 150.876° SSE |
| 4 mins | 2026-09-18 02:26:27.423Z | 163.68° S | 2026-09-18 02:28:27.423Z | 118.026° SE | 22.757° | 2026-09-18 02:30:27.423Z | 82.306° E |
| 5 mins | 2026-09-18 04:04:27.423Z | 264.728° W | 2026-09-18 04:06:27.423Z | 326.147° NNW | 44.91° | 2026-09-18 04:09:27.423Z | 36.324° NE |
| 5 mins | 2026-09-18 09:03:27.423Z | 339.229° N | 2026-09-18 09:05:27.423Z | 22.31° NNE | 27.894° | 2026-09-18 09:08:27.423Z | 83.905° E |
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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