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
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 SPACEMOBILE-006
1 67232U 25309A 26137.37093071 .00000615 00000-0 45010-4 0 9994
2 67232 52.9957 112.7589 0011893 42.5532 317.6381 15.18353939 21914Epoch: 2026-05-17T08:54Z
TLE epoch observation values (Epoch: 2026-05-17T08:54:08.413Z)
Latitude
-0.00001°
Longitude
104.14933°
Altitude
505.643 km
Speed
7.616 km/s
True Right ascension
07h 31m 02s
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
12:51:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
519.29 km
Perigee altitude
502.903 km
Semi-major axis
6,889.234 km
Eccentricity
0.00119
Inclination
52.9957°
RAAN
112.7589°
Arg. of periapsis
42.5532°
True anomaly
317.54617°
Mean anomaly
317.6381°
Eccentric anomaly
317.59214°
Mean motion
3.79566 °/min
Orbital period
94.85 mins
BSTAR
0.00004501
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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 | 2026-05-18 07:30:59.646Z | 320.327° NNW | 2026-05-18 07:33:59.646Z | 69.623° E | 39.607° | 2026-05-18 07:36:59.646Z | 116.674° SE |
| 6 mins | 2026-05-19 00:34:59.646Z | 216.771° SW | 2026-05-19 00:36:59.646Z | 173.525° S | 42.139° | 2026-05-19 00:40:59.646Z | 54.781° ENE |
| 4 mins | 2026-05-19 02:14:59.646Z | 305.997° NW | 2026-05-19 02:15:59.646Z | 327.65° NNW | 20.641° | 2026-05-19 02:18:59.646Z | 24.881° 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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