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: 10 hours ago
TLE from 10 hours ago
0 SPACEMOBILE-001
1 61047U 24163C 26171.42003137 .00003361 00000-0 16486-3 0 9992
2 61047 52.9746 294.2310 0008880 119.9533 240.2344 15.20841656 98250Epoch: 2026-06-20T10:04Z
TLE epoch observation values (Epoch: 2026-06-20T10:04:50.710Z)
Latitude
-0.00001°
Longitude
-125.61521°
Altitude
507.214 km
Speed
7.61 km/s
True Right ascension
19h 36m 55s
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
07:24:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.697 km
Perigee altitude
497.475 km
Semi-major axis
6,881.723 km
Eccentricity
0.00089
Inclination
52.9746°
RAAN
294.231°
Arg. of periapsis
119.9533°
True anomaly
240.14612°
Mean anomaly
240.2344°
Eccentric anomaly
240.19025°
Mean motion
3.80187 °/min
Orbital period
94.69 mins
BSTAR
0.00016486
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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 | 2026-06-21 09:53:19.461Z | 183.162° SSW | 2026-06-21 09:56:19.461Z | 126.17° SE | 22.608° | 2026-06-21 09:58:19.461Z | 85.283° E |
| 5 mins | 2026-06-21 11:32:19.461Z | 264.262° W | 2026-06-21 11:34:19.461Z | 316.102° NNW | 33.87° | 2026-06-21 11:37:19.461Z | 34.153° NE |
| 5 mins | 2026-06-21 16:31:19.461Z | 340.772° N | 2026-06-21 16:33:19.461Z | 28.169° NE | 25.827° | 2026-06-21 16:36:19.461Z | 87.614° E |
| 5 mins | 2026-06-21 18:10:19.461Z | 279.519° WNW | 2026-06-21 18:12:19.461Z | 209.362° SW | 33.064° | 2026-06-21 18:15:19.461Z | 155.761° SSE |
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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