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: 1 day ago
TLE from 1 day ago
0 SPACEMOBILE-001
1 61047U 24163C 26259.03003112 -.00000563 00000-0 -10653-4 0 9993
2 61047 52.9701 251.4354 0007787 40.7296 319.4279 15.20391114111583Epoch: 2026-09-16T00:43Z
TLE epoch observation values (Epoch: 2026-09-16T00:43:14.688Z)
Latitude
-0.00003°
Longitude
-114.36331°
Altitude
501.466 km
Speed
7.617 km/s
True Right ascension
16h 45m 44s
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
02:02:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.306 km
Perigee altitude
499.586 km
Semi-major axis
6,883.083 km
Eccentricity
0.00078
Inclination
52.9701°
RAAN
251.4354°
Arg. of periapsis
40.7296°
True anomaly
319.36982°
Mean anomaly
319.4279°
Eccentric anomaly
319.39886°
Mean motion
3.80074 °/min
Orbital period
94.72 mins
BSTAR
-0.000010653
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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 | 2026-09-18 01:49:02.068Z | 225.037° WSW | 2026-09-18 01:51:02.068Z | 209.513° SW | 68.209° | 2026-09-18 01:55:02.068Z | 51.909° ENE |
| 4 mins | 2026-09-18 03:29:02.068Z | 308.077° NW | 2026-09-18 03:30:02.068Z | 328.259° NNW | 20.262° | 2026-09-18 03:33:02.068Z | 23.672° NE |
| 6 mins | 2026-09-18 08:27:02.068Z | 316.502° NNW | 2026-09-18 08:29:02.068Z | 12.852° NNE | 73.306° | 2026-09-18 08:33:02.068Z | 124.751° SE |
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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