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: 1 day ago
TLE from 1 day ago
0 SPACEMOBILE-001
1 61047U 24163C 26034.87394516 .00001437 00000-0 78416-4 0 9997
2 61047 52.9736 202.3285 0010939 89.5945 270.6303 15.21100120 77475Epoch: 2026-02-03T20:58Z
TLE epoch observation values (Epoch: 2026-02-03T20:58:28.861Z)
Latitude
-0.00002°
Longitude
113.65961°
Altitude
503.323 km
Speed
7.614 km/s
True Right ascension
13h 29m 18s
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
06:44:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.334 km
Perigee altitude
495.279 km
Semi-major axis
6,880.943 km
Eccentricity
0.00109
Inclination
52.9736°
RAAN
202.3285°
Arg. of periapsis
89.5945°
True anomaly
270.50495°
Mean anomaly
270.6303°
Eccentric anomaly
270.56763°
Mean motion
3.80252 °/min
Orbital period
94.67 mins
BSTAR
0.000078416
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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 | 2026-02-05 12:33:16.907Z | 182.32° SSW | 2026-02-05 12:36:16.907Z | 117.809° SE | 23.374° | 2026-02-05 12:38:16.907Z | 80.088° E |
| 5 mins | 2026-02-05 14:12:16.907Z | 270.593° WNW | 2026-02-05 14:14:16.907Z | 330.661° NNW | 32.685° | 2026-02-05 14:17:16.907Z | 35.37° NE |
| 5 mins | 2026-02-05 19:11:16.907Z | 345.657° N | 2026-02-05 19:13:16.907Z | 40.144° NE | 26.396° | 2026-02-05 19:16:16.907Z | 92.34° ESE |
| 5 mins | 2026-02-05 20:49:16.907Z | 285.534° WNW | 2026-02-05 20:51:16.907Z | 236.513° WSW | 31.776° | 2026-02-05 20:54:16.907Z | 162.255° 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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