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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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: 9 hours ago
TLE from 9 hours ago
0 SPACEMOBILE-001
1 61047U 24163C 26253.50840734 -.00000797 00000-0 -21195-4 0 9990
2 61047 52.9713 276.8144 0007132 26.8263 333.3099 15.20472422110741Epoch: 2026-09-10T12:12Z
TLE epoch observation values (Epoch: 2026-09-10T12:12:06.394Z)
Latitude
0.00003°
Longitude
104.24267°
Altitude
500.905 km
Speed
7.618 km/s
True Right ascension
18h 27m 15s
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
13:49:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.609 km
Perigee altitude
499.792 km
Semi-major axis
6,882.837 km
Eccentricity
0.00071
Inclination
52.9713°
RAAN
276.8144°
Arg. of periapsis
26.8263°
True anomaly
333.27316°
Mean anomaly
333.3099°
Eccentric anomaly
333.29153°
Mean motion
3.80095 °/min
Orbital period
94.71 mins
BSTAR
-0.000021195
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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 | 2026-09-11 04:08:25.091Z | 216.454° SW | 2026-09-11 04:12:25.091Z | 97.928° ESE | 55.035° | 2026-09-11 04:15:25.091Z | 57.066° ENE |
| 4 mins | 2026-09-11 05:49:25.091Z | 303.625° NW | 2026-09-11 05:50:25.091Z | 326.047° NNW | 23.543° | 2026-09-11 05:53:25.091Z | 25.032° NE |
| 6 mins | 2026-09-11 10:47:25.091Z | 324.483° NNW | 2026-09-11 10:49:25.091Z | 22.912° NE | 56.591° | 2026-09-11 10:53:25.091Z | 116.291° SE |
| 4 mins | 2026-09-11 12:26:25.091Z | 259.156° W | 2026-09-11 12:27:25.091Z | 240.678° WSW | 17.796° | 2026-09-11 12:30:25.091Z | 189.16° 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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