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 26228.46572875 .00001226 00000-0 70108-4 0 9999
2 61047 52.9739 31.9252 0005078 313.9115 46.1460 15.20494869106938Epoch: 2026-08-16T11:10Z
TLE epoch observation values (Epoch: 2026-08-16T11:10:38.963Z)
Latitude
-0°
Longitude
-100.599°
Altitude
502.802 km
Speed
7.615 km/s
True Right ascension
02h 07m 42s
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
10:48:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.127 km
Perigee altitude
501.137 km
Semi-major axis
6,882.769 km
Eccentricity
0.00051
Inclination
52.9739°
RAAN
31.9252°
Arg. of periapsis
313.9115°
True anomaly
46.18798°
Mean anomaly
46.146°
Eccentric anomaly
46.16699°
Mean motion
3.801 °/min
Orbital period
94.71 mins
BSTAR
0.000070108
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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 | 2026-08-16 21:09:38.104Z | 297.65° NW | 2026-08-16 21:12:38.104Z | 241.008° WSW | 36.067° | 2026-08-16 21:16:38.104Z | 150.505° SSE |
| 4 mins | 2026-08-17 12:35:38.104Z | 157.064° SSE | 2026-08-17 12:36:38.104Z | 134.443° SE | 21.236° | 2026-08-17 12:39:38.104Z | 79.015° E |
| 6 mins | 2026-08-17 14:12:38.104Z | 258.348° W | 2026-08-17 14:15:38.104Z | 348.368° N | 34.482° | 2026-08-17 14:18:38.104Z | 39.328° NE |
| 4 mins | 2026-08-17 19:12:38.104Z | 351.143° N | 2026-08-17 19:13:38.104Z | 15.117° NNE | 24.708° | 2026-08-17 19:16:38.104Z | 81.356° E |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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