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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SPACEMOBILE-001 radio frequencies
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Edit Public Description
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, 4.5 m
Radar Cross Section
1.500 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 SPACEMOBILE-001
1 61047U 24163C 25258.06821180 .00004150 00000-0 20102-3 0 9990
2 61047 52.9716 134.5954 0011854 23.7347 336.4192 15.20661622 55892Epoch: 2025-09-15T01:38Z
TLE epoch observation values (Epoch: 2025-09-15T01:38:13.499Z)
Latitude
0.00001°
Longitude
115.76098°
Altitude
497.245 km
Speed
7.621 km/s
True Right ascension
08h 58m 22s
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
07:27:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.288 km
Perigee altitude
495.971 km
Semi-major axis
6,882.266 km
Eccentricity
0.00119
Inclination
52.9716°
RAAN
134.5954°
Arg. of periapsis
23.7347°
True anomaly
336.36479°
Mean anomaly
336.4192°
Eccentric anomaly
336.392°
Mean motion
3.80142 °/min
Orbital period
94.7 mins
BSTAR
0.00020102
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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 | 2025-09-15 17:33:47.542Z | 175.638° S | 2025-09-15 17:35:47.542Z | 140.973° SSE | 19.691° | 2025-09-15 17:38:47.542Z | 82.921° E |
| 5 mins | 2025-09-15 19:12:47.542Z | 264.35° W | 2025-09-15 19:14:47.542Z | 336.145° NNW | 36.088° | 2025-09-15 19:17:47.542Z | 38.664° NE |
| 4 mins | 2025-09-16 00:11:47.542Z | 348.018° N | 2025-09-16 00:13:47.542Z | 38.082° NE | 24.125° | 2025-09-16 00:15:47.542Z | 77.926° E |
| 6 mins | 2025-09-16 01:49:47.542Z | 291.768° WNW | 2025-09-16 01:51:47.542Z | 243.683° WSW | 36.09° | 2025-09-16 01:55:47.542Z | 150.29° SSE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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