SPACEMOBILE-005, 61046
Orbit data source: Space-Track
SPACEMOBILE-005, 61046 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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61046 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: 1 day ago
TLE from 1 day ago
0 SPACEMOBILE-005
1 61046U 24163B 25317.74224476 .00011032 00000-0 50421-3 0 9999
2 61046 52.9738 220.3642 0009708 185.2605 174.8289 15.21026097 64971Epoch: 2025-11-13T17:48Z
TLE epoch observation values (Epoch: 2025-11-13T17:48:49.947Z)
Latitude
-0°
Longitude
-99.93964°
Altitude
510.273 km
Speed
7.606 km/s
True Right ascension
14h 41m 27s
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
17:11:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.71 km
Perigee altitude
496.349 km
Semi-major axis
6,881.167 km
Eccentricity
0.00097
Inclination
52.9738°
RAAN
220.3642°
Arg. of periapsis
185.2605°
True anomaly
174.83891°
Mean anomaly
174.8289°
Eccentric anomaly
174.83391°
Mean motion
3.80233 °/min
Orbital period
94.68 mins
BSTAR
0.00050421
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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-005 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 | 2025-11-14 20:49:32.381Z | 252.11° W | 2025-11-14 20:52:32.381Z | 317.157° NNW | 36.756° | 2025-11-14 20:55:32.381Z | 36.904° NE |
| 5 mins | 2025-11-15 01:49:32.381Z | 343.653° N | 2025-11-15 01:51:32.381Z | 30.132° NE | 24.109° | 2025-11-15 01:54:32.381Z | 85.032° E |
| 6 mins | 2025-11-15 03:27:32.381Z | 294.335° NW | 2025-11-15 03:30:32.381Z | 201.469° SSW | 36.014° | 2025-11-15 03:33:32.381Z | 150.6° SSE |
| 4 mins | 2025-11-15 18:52:32.381Z | 155.095° SSE | 2025-11-15 18:53:32.381Z | 132.878° SE | 20.705° | 2025-11-15 18:56:32.381Z | 79.181° E |
| 6 mins | 2025-11-15 20:29:32.381Z | 257.772° W | 2025-11-15 20:31:32.381Z | 301.737° NW | 35.175° | 2025-11-15 20:35:32.381Z | 40.281° 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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