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: 8 hours ago
TLE from 8 hours ago
0 SPACEMOBILE-001
1 61047U 24163C 26073.57384834 .00022667 00000-0 10185-2 0 9994
2 61047 52.9695 24.2895 0007661 193.2954 166.7840 15.21052295 83363Epoch: 2026-03-14T13:46Z
TLE epoch observation values (Epoch: 2026-03-14T13:46:20.496Z)
Latitude
0.00001°
Longitude
5.51103°
Altitude
508.673 km
Speed
7.608 km/s
True Right ascension
01h 37m 09s
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
02:16:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.223 km
Perigee altitude
497.68 km
Semi-major axis
6,881.088 km
Eccentricity
0.00077
Inclination
52.9695°
RAAN
24.2895°
Arg. of periapsis
193.2954°
True anomaly
166.80405°
Mean anomaly
166.784°
Eccentric anomaly
166.79403°
Mean motion
3.8024 °/min
Orbital period
94.68 mins
BSTAR
0.0010185
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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 | 2026-03-14 23:24:46.028Z | 222.915° SW | 2026-03-14 23:27:46.028Z | 138.79° SSE | 44.236° | 2026-03-14 23:30:46.028Z | 54.012° ENE |
| 4 mins | 2026-03-15 01:04:46.028Z | 298.484° NW | 2026-03-15 01:06:46.028Z | 338.998° N | 20.077° | 2026-03-15 01:08:46.028Z | 17.667° NNE |
| 4 mins | 2026-03-15 04:24:46.028Z | 352.009° N | 2026-03-15 04:25:46.028Z | 10.364° NNE | 16.541° | 2026-03-15 04:28:46.028Z | 62.09° ENE |
| 6 mins | 2026-03-15 06:02:46.028Z | 316.418° NNW | 2026-03-15 06:05:46.028Z | 88.481° E | 41.315° | 2026-03-15 06:08:46.028Z | 122.366° SE |
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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