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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Edit Public Description
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: 11 hours ago
TLE from 11 hours ago
0 SPACEMOBILE-001
1 61047U 24163C 25310.57841037 .00008255 00000-0 38178-3 0 9990
2 61047 52.9675 253.1305 0009793 166.2661 193.8601 15.20964819 63887Epoch: 2025-11-06T13:52Z
TLE epoch observation values (Epoch: 2025-11-06T13:52:54.655Z)
Latitude
-0.00008°
Longitude
-1.132°
Altitude
510.347 km
Speed
7.606 km/s
True Right ascension
16h 52m 31s
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
21:24:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.954 km
Perigee altitude
496.477 km
Semi-major axis
6,881.353 km
Eccentricity
0.00098
Inclination
52.9675°
RAAN
253.1305°
Arg. of periapsis
166.2661°
True anomaly
193.83325°
Mean anomaly
193.8601°
Eccentric anomaly
193.84667°
Mean motion
3.80218 °/min
Orbital period
94.68 mins
BSTAR
0.00038178
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-07 04:32:20.401Z | 346.149° N | 2025-11-07 04:34:20.401Z | 29.434° NE | 21.192° | 2025-11-07 04:36:20.401Z | 68.879° E |
| 6 mins | 2025-11-07 06:10:20.401Z | 301.367° NW | 2025-11-07 06:13:20.401Z | 187.456° SSW | 41.05° | 2025-11-07 06:16:20.401Z | 141.795° SSE |
| 6 mins | 2025-11-07 23:12:20.401Z | 247.531° W | 2025-11-07 23:15:20.401Z | 0.276° NNE | 38.97° | 2025-11-07 23:18:20.401Z | 43.486° NE |
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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