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: 15 hours ago
TLE from 15 hours ago
0 SPACEMOBILE-001
1 61047U 24163C 26125.54872632 .00000558 00000-0 39630-4 0 9990
2 61047 52.9760 145.1818 0007628 2.1393 357.9633 15.20842617 91279Epoch: 2026-05-05T13:10Z
TLE epoch observation values (Epoch: 2026-05-05T13:10:09.954Z)
Latitude
0.00003°
Longitude
84.21837°
Altitude
498.928 km
Speed
7.619 km/s
True Right ascension
09h 40m 43s
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
12:03:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.832 km
Perigee altitude
498.333 km
Semi-major axis
6,881.72 km
Eccentricity
0.00076
Inclination
52.976°
RAAN
145.1818°
Arg. of periapsis
2.1393°
True anomaly
357.96019°
Mean anomaly
357.9633°
Eccentric anomaly
357.96175°
Mean motion
3.80187 °/min
Orbital period
94.69 mins
BSTAR
0.00003963
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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 | 2026-05-06 05:10:26.998Z | 274.759° WNW | 2026-05-06 05:13:26.998Z | 340.294° N | 25.845° | 2026-05-06 05:16:26.998Z | 32.944° NE |
| 6 mins | 2026-05-06 10:09:26.998Z | 328.188° NNW | 2026-05-06 10:12:26.998Z | 54.8° ENE | 32.926° | 2026-05-06 10:15:26.998Z | 105.015° ESE |
| 5 mins | 2026-05-06 11:48:26.998Z | 271.452° WNW | 2026-05-06 11:50:26.998Z | 227.3° WSW | 23.02° | 2026-05-06 11:53:26.998Z | 174.308° S |
| 6 mins | 2026-05-07 03:11:26.998Z | 199.915° SSW | 2026-05-07 03:14:26.998Z | 115.329° SE | 33.4° | 2026-05-07 03:17:26.998Z | 63.496° ENE |
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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