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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 SPACEMOBILE-006
1 67232U 25309A 26187.12895901 .00001618 00000-0 92409-4 0 9992
2 67232 52.9956 244.8687 0010703 185.6932 174.3942 15.18641469 29479Epoch: 2026-07-06T03:05Z
TLE epoch observation values (Epoch: 2026-07-06T03:05:42.058Z)
Latitude
0.00001°
Longitude
-85.67491°
Altitude
518.16 km
Speed
7.602 km/s
True Right ascension
16h 19m 28s
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
05:56:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
517.6 km
Perigee altitude
502.854 km
Semi-major axis
6,888.364 km
Eccentricity
0.00107
Inclination
52.9956°
RAAN
244.8687°
Arg. of periapsis
185.6932°
True anomaly
174.40616°
Mean anomaly
174.3942°
Eccentric anomaly
174.40018°
Mean motion
3.79637 °/min
Orbital period
94.83 mins
BSTAR
0.000092409
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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 | 2026-07-07 06:06:21.649Z | 212.324° SW | 2026-07-07 06:10:21.649Z | 106.891° ESE | 37.615° | 2026-07-07 06:13:21.649Z | 59.587° ENE |
| 4 mins | 2026-07-07 07:47:21.649Z | 298.926° NW | 2026-07-07 07:48:21.649Z | 321.614° NNW | 23.226° | 2026-07-07 07:51:21.649Z | 24.452° NE |
| 6 mins | 2026-07-07 12:45:21.649Z | 322.903° NNW | 2026-07-07 12:48:21.649Z | 55.874° ENE | 37.612° | 2026-07-07 12:51:21.649Z | 111.434° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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