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.
Focus sentinelFocus sentinel
Request partner network tasking
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
67232 intel report (Beta)
Focus sentinelFocus sentinel
Edit Public Description
Focus sentinelFocus sentinel
Edit Sat Name
Focus sentinelFocus sentinel
Create New Watchlist
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: 7 hours ago
TLE from 7 hours ago
0 SPACEMOBILE-006
1 67232U 25309A 26232.60230639 .00002756 00000-0 14594-3 0 9999
2 67232 52.9972 36.5277 0010219 340.4064 19.6536 15.18794563 36389Epoch: 2026-08-20T14:27Z
TLE epoch observation values (Epoch: 2026-08-20T14:27:19.272Z)
Latitude
0.00003°
Longitude
-149.24164°
Altitude
503.733 km
Speed
7.617 km/s
True Right ascension
02h 26m 06s
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
12:13:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.803 km
Perigee altitude
502.725 km
Semi-major axis
6,887.901 km
Eccentricity
0.00102
Inclination
52.9972°
RAAN
36.5277°
Arg. of periapsis
340.4064°
True anomaly
19.69303°
Mean anomaly
19.6536°
Eccentric anomaly
19.67331°
Mean motion
3.79676 °/min
Orbital period
94.82 mins
BSTAR
0.00014594
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #309 in the year 2025 (2025-12-24 UTC)
Did you know?
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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-20 21:17:13.758Z | 298.106° NW | 2026-08-20 21:21:13.758Z | 206.32° SW | 34.682° | 2026-08-20 21:24:13.758Z | 153.853° SSE |
| 4 mins | 2026-08-21 12:44:13.758Z | 166.585° S | 2026-08-21 12:46:13.758Z | 119.147° SE | 22.516° | 2026-08-21 12:48:13.758Z | 81.826° E |
| 5 mins | 2026-08-21 14:22:13.758Z | 266.107° W | 2026-08-21 14:24:13.758Z | 322.33° NNW | 34.106° | 2026-08-21 14:27:13.758Z | 34.886° NE |
| 5 mins | 2026-08-21 19:21:13.758Z | 336.544° NNW | 2026-08-21 19:23:13.758Z | 18.362° NNE | 26.218° | 2026-08-21 19:26:13.758Z | 84.689° E |
| 5 mins | 2026-08-21 21:00:13.758Z | 285.498° WNW | 2026-08-21 21:02:13.758Z | 231.091° WSW | 33.833° | 2026-08-21 21:05:13.758Z | 159.357° 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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
|---|