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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Edit Public Description
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
RCS unknown
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 SPACEMOBILE-006
1 67232U 25309A 26014.19053270 .00000005 00000-0 15926-4 0 9991
2 67232 52.9988 316.5407 0011945 26.8655 333.2955 15.17741212 3207Epoch: 2026-01-14T04:34Z
TLE epoch observation values (Epoch: 2026-01-14T04:34:22.025Z)
Latitude
0.00003°
Longitude
134.28688°
Altitude
506.196 km
Speed
7.616 km/s
True Right ascension
21h 06m 09s
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
18:29:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.181 km
Perigee altitude
504.719 km
Semi-major axis
6,891.087 km
Eccentricity
0.00119
Inclination
52.9988°
RAAN
316.5407°
Arg. of periapsis
26.8655°
True anomaly
333.23391°
Mean anomaly
333.2955°
Eccentric anomaly
333.26471°
Mean motion
3.79412 °/min
Orbital period
94.88 mins
BSTAR
0.000015926
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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 | 2026-01-14 22:07:02.123Z | 196.384° SSW | 2026-01-14 22:10:02.123Z | 128.731° SE | 30.81° | 2026-01-14 22:13:02.123Z | 68.178° E |
| 5 mins | 2026-01-14 23:47:02.123Z | 285.46° WNW | 2026-01-14 23:49:02.123Z | 341.519° N | 27.53° | 2026-01-14 23:52:02.123Z | 34.063° NE |
| 5 mins | 2026-01-15 04:46:02.123Z | 334.632° NNW | 2026-01-15 04:48:02.123Z | 27.633° NE | 32.253° | 2026-01-15 04:51:02.123Z | 97.818° ESE |
| 5 mins | 2026-01-15 06:25:02.123Z | 271.039° WNW | 2026-01-15 06:27:02.123Z | 221.752° SW | 25.287° | 2026-01-15 06:30:02.123Z | 169.779° S |
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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