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, 5.0 m
Radar Cross Section
24.992 m²
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 SPACEMOBILE-006
1 67232U 25309A 26089.38277572 .00002301 00000-0 12661-3 0 9990
2 67232 52.9968 332.4688 0009513 246.9768 113.0222 15.18156507 14628Epoch: 2026-03-30T09:11Z
TLE epoch observation values (Epoch: 2026-03-30T09:11:11.822Z)
Latitude
-0.00004°
Longitude
6.8944°
Altitude
514.858 km
Speed
7.606 km/s
True Right ascension
22h 09m 52s
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
22:05:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
518.248 km
Perigee altitude
505.139 km
Semi-major axis
6,889.831 km
Eccentricity
0.00095
Inclination
52.9968°
RAAN
332.4688°
Arg. of periapsis
246.9768°
True anomaly
113.12248°
Mean anomaly
113.0222°
Eccentric anomaly
113.07235°
Mean motion
3.79516 °/min
Orbital period
94.86 mins
BSTAR
0.00012661
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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 | 2026-03-30 18:50:40.560Z | 219.037° SW | 2026-03-30 18:53:40.560Z | 122.692° SE | 43.153° | 2026-03-30 18:56:40.560Z | 55.771° ENE |
| 5 mins | 2026-03-30 20:30:40.560Z | 296.089° NW | 2026-03-30 20:32:40.560Z | 337.174° NNW | 21.286° | 2026-03-30 20:35:40.560Z | 28.715° NE |
| 6 mins | 2026-03-31 01:29:40.560Z | 320.123° NNW | 2026-03-31 01:31:40.560Z | 13.884° NNE | 41.984° | 2026-03-31 01:35:40.560Z | 120.454° SE |
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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