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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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, 6.5 m
Radar Cross Section
32.590 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 SPACEMOBILE-001
1 61047U 24163C 25347.96611705 .00018007 00000-0 81212-3 0 9993
2 61047 52.9753 81.1452 0007665 293.0400 66.9785 15.21074895 69574Epoch: 2025-12-13T23:11Z
TLE epoch observation values (Epoch: 2025-12-13T23:11:12.513Z)
Latitude
-0.00006°
Longitude
10.45721°
Altitude
501.414 km
Speed
7.616 km/s
True Right ascension
05h 24m 34s
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
15:57:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.157 km
Perigee altitude
497.608 km
Semi-major axis
6,881.019 km
Eccentricity
0.00077
Inclination
52.9753°
RAAN
81.1452°
Arg. of periapsis
293.04°
True anomaly
67.05937°
Mean anomaly
66.9785°
Eccentric anomaly
67.01893°
Mean motion
3.80245 °/min
Orbital period
94.68 mins
BSTAR
0.00081212
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-15 08:27:43.091Z | 209.731° SW | 2025-12-15 08:30:43.091Z | 158.293° S | 36.478° | 2025-12-15 08:34:43.091Z | 60.171° ENE |
| 5 mins | 2025-12-15 10:07:43.091Z | 286.588° WNW | 2025-12-15 10:09:43.091Z | 330.212° NNW | 24.134° | 2025-12-15 10:12:43.091Z | 28.56° NE |
| 5 mins | 2025-12-15 15:06:43.091Z | 332.177° NNW | 2025-12-15 15:08:43.091Z | 43.732° NE | 36.962° | 2025-12-15 15:11:43.091Z | 108.335° ESE |
| 4 mins | 2025-12-15 16:45:43.091Z | 255.643° W | 2025-12-15 16:46:43.091Z | 233.958° WSW | 19.998° | 2025-12-15 16:49:43.091Z | 181.317° SSW |
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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