SPACEMOBILE-001, 61047
Orbit data source: Space-Track
SPACEMOBILE-001, 61047 is a payload satellite owned by AST & Science (US) in LEO that was launched on Thu, 12 Sep 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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61047 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
AST & Science
Mission
Operational Commercial Communications
Bus & Motor
BW3, Unknown motor
Mass
1,500 kg wet, 1,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Plate, 6.5 m
Radar Cross Section
32.590 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 SPACEMOBILE-001
1 61047U 24163C 26282.62868136 .00000737 00000-0 48192-4 0 9999
2 61047 52.9724 142.9704 0008733 96.7117 263.4871 15.20432396115179Epoch: 2026-10-09T15:05Z
TLE epoch observation values (Epoch: 2026-10-09T15:05:18.069Z)
Latitude
-0.00003°
Longitude
-101.60234°
Altitude
506.098 km
Speed
7.612 km/s
True Right ascension
09h 31m 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
00:38:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.832 km
Perigee altitude
498.81 km
Semi-major axis
6,882.958 km
Eccentricity
0.00087
Inclination
52.9724°
RAAN
142.9704°
Arg. of periapsis
96.7117°
True anomaly
263.38769°
Mean anomaly
263.4871°
Eccentric anomaly
263.43739°
Mean motion
3.80085 °/min
Orbital period
94.72 mins
BSTAR
0.000048192
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Other satellites on launch #163 in the year 2024 (2024-09-12 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-001 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-11 16:09:09.711Z | 180.199° SSW | 2026-10-11 16:11:09.711Z | 141.763° SSE | 25.725° | 2026-10-11 16:14:09.711Z | 78.903° E |
| 5 mins | 2026-10-11 17:48:09.711Z | 271.465° WNW | 2026-10-11 17:50:09.711Z | 334.522° NNW | 40.514° | 2026-10-11 17:53:09.711Z | 35.925° NE |
| 5 mins | 2026-10-11 22:47:09.711Z | 344.919° N | 2026-10-11 22:49:09.711Z | 37.307° NE | 29.67° | 2026-10-11 22:52:09.711Z | 90.928° ESE |
| 5 mins | 2026-10-12 00:25:09.711Z | 287.808° WNW | 2026-10-12 00:27:09.711Z | 242.614° WSW | 39.099° | 2026-10-12 00:30:09.711Z | 162.387° 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 |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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