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: 11 hours ago
TLE from 11 hours ago
0 SPACEMOBILE-001
1 61047U 24163C 25340.60690025 .00019541 00000-0 88112-3 0 9999
2 61047 52.9771 114.9948 0007204 266.9011 93.1159 15.21029539 68453Epoch: 2025-12-06T14:33Z
TLE epoch observation values (Epoch: 2025-12-06T14:33:56.181Z)
Latitude
-0.00004°
Longitude
-179.12153°
Altitude
503.883 km
Speed
7.613 km/s
True Right ascension
07h 39m 58s
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
23:27:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.976 km
Perigee altitude
498.062 km
Semi-major axis
6,881.156 km
Eccentricity
0.00072
Inclination
52.9771°
RAAN
114.9948°
Arg. of periapsis
266.9011°
True anomaly
93.19833°
Mean anomaly
93.1159°
Eccentric anomaly
93.15711°
Mean motion
3.80234 °/min
Orbital period
94.68 mins
BSTAR
0.00088112
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-07 11:13:54.145Z | 197.5° SSW | 2025-12-07 11:16:54.145Z | 120.644° SE | 32.143° | 2025-12-07 11:19:54.145Z | 65.585° ENE |
| 5 mins | 2025-12-07 12:52:54.145Z | 278.152° WNW | 2025-12-07 12:54:54.145Z | 321.534° NNW | 26.744° | 2025-12-07 12:57:54.145Z | 28.124° NE |
| 5 mins | 2025-12-07 17:51:54.145Z | 333.766° NNW | 2025-12-07 17:53:54.145Z | 28.83° NE | 33.173° | 2025-12-07 17:56:54.145Z | 99.896° ESE |
| 4 mins | 2025-12-07 19:30:54.145Z | 265.302° W | 2025-12-07 19:31:54.145Z | 242.649° WSW | 23.435° | 2025-12-07 19:34:54.145Z | 178.346° 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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