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 25312.81398130 .00007941 00000-0 36816-3 0 9997
2 61046 52.9718 243.0336 0010207 170.8842 189.2339 15.20930987 64225Epoch: 2025-11-08T19:32Z
TLE epoch observation values (Epoch: 2025-11-08T19:32:07.984Z)
Latitude
-0.00004°
Longitude
-98.2379°
Altitude
510.84 km
Speed
7.606 km/s
True Right ascension
16h 12m 08s
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
18:23:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.341 km
Perigee altitude
496.293 km
Semi-major axis
6,881.454 km
Eccentricity
0.00102
Inclination
52.9718°
RAAN
243.0336°
Arg. of periapsis
170.8842°
True anomaly
189.21516°
Mean anomaly
189.2339°
Eccentric anomaly
189.22453°
Mean motion
3.80209 °/min
Orbital period
94.68 mins
BSTAR
0.00036816
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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 | 2025-11-09 22:32:57.537Z | 248.975° W | 2025-11-09 22:35:57.537Z | 335.834° NNW | 39.209° | 2025-11-09 22:38:57.537Z | 40.879° NE |
| 4 mins | 2025-11-10 03:32:57.537Z | 349.729° N | 2025-11-10 03:34:57.537Z | 36.995° NE | 22.072° | 2025-11-10 03:36:57.537Z | 74.605° E |
| 6 mins | 2025-11-10 05:10:57.537Z | 296.555° NW | 2025-11-10 05:12:57.537Z | 249.332° W | 39.212° | 2025-11-10 05:16:57.537Z | 144.954° SSE |
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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