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: 9 hours ago
TLE from 9 hours ago
0 SPACEMOBILE-006
1 67232U 25309A 26043.88816586 .00002452 00000-0 13508-3 0 9997
2 67232 52.9937 180.6743 0012365 109.5050 250.7280 15.17840496 7717Epoch: 2026-02-12T21:18Z
TLE epoch observation values (Epoch: 2026-02-12T21:18:57.530Z)
Latitude
-0°
Longitude
78.00112°
Altitude
516.067 km
Speed
7.605 km/s
True Right ascension
12h 02m 41s
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
08:43:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.171 km
Perigee altitude
504.13 km
Semi-major axis
6,890.787 km
Eccentricity
0.00124
Inclination
52.9937°
RAAN
180.6743°
Arg. of periapsis
109.505°
True anomaly
250.59432°
Mean anomaly
250.728°
Eccentric anomaly
250.66115°
Mean motion
3.79437 °/min
Orbital period
94.88 mins
BSTAR
0.00013508
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-13 11:42:47.200Z | 223.436° SW | 2026-02-13 11:45:47.200Z | 184.264° SSW | 43.554° | 2026-02-13 11:49:47.200Z | 53.002° ENE |
| 4 mins | 2026-02-13 13:23:47.200Z | 307.249° NW | 2026-02-13 13:24:47.200Z | 327.953° NNW | 19.759° | 2026-02-13 13:27:47.200Z | 24.14° NE |
| 6 mins | 2026-02-13 18:21:47.200Z | 315.756° NNW | 2026-02-13 18:24:47.200Z | 83.479° E | 42.268° | 2026-02-13 18:27:47.200Z | 122.697° 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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