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: 22 hours ago
TLE from 22 hours ago
0 SPACEMOBILE-001
1 61047U 24163C 25257.41097238 .00003963 00000-0 19264-3 0 9995
2 61047 52.9706 137.6167 0011873 21.0280 339.1200 15.20663759 55791Epoch: 2025-09-14T09:51Z
TLE epoch observation values (Epoch: 2025-09-14T09:51:48.013Z)
Latitude
-0.00003°
Longitude
-3.96375°
Altitude
497.08 km
Speed
7.622 km/s
True Right ascension
09h 10m 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
00:49:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.294 km
Perigee altitude
495.952 km
Semi-major axis
6,882.26 km
Eccentricity
0.00119
Inclination
52.9706°
RAAN
137.6167°
Arg. of periapsis
21.028°
True anomaly
339.07144°
Mean anomaly
339.12°
Eccentric anomaly
339.09573°
Mean motion
3.80143 °/min
Orbital period
94.7 mins
BSTAR
0.00019264
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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 17:34:02.403Z | 172.476° S | 2025-09-15 17:36:02.403Z | 134.907° SE | 20.043° | 2025-09-15 17:39:02.403Z | 80.119° E |
| 6 mins | 2025-09-15 19:12:02.403Z | 256.574° W | 2025-09-15 19:15:02.403Z | 349.484° N | 35.08° | 2025-09-15 19:18:02.403Z | 39.993° NE |
| 4 mins | 2025-09-16 00:12:02.403Z | 352.882° N | 2025-09-16 00:13:02.403Z | 17.048° NNE | 24.127° | 2025-09-16 00:16:02.403Z | 80.929° E |
| 5 mins | 2025-09-16 01:50:02.403Z | 289.253° WNW | 2025-09-16 01:52:02.403Z | 229.296° WSW | 36.778° | 2025-09-16 01:55:02.403Z | 153.827° 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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