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: 8 hours ago
TLE from 8 hours ago
0 SPACEMOBILE-005
1 61046U 24163B 25343.63122880 .00022604 00000-0 10145-2 0 9997
2 61046 52.9800 101.2854 0008699 276.7360 83.2644 15.21087557 68919Epoch: 2025-12-09T15:08Z
TLE epoch observation values (Epoch: 2025-12-09T15:08:58.168Z)
Latitude
-0.00004°
Longitude
155.42986°
Altitude
502.739 km
Speed
7.615 km/s
True Right ascension
06h 45m 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
21:18:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.829 km
Perigee altitude
496.858 km
Semi-major axis
6,880.98 km
Eccentricity
0.00087
Inclination
52.98°
RAAN
101.2854°
Arg. of periapsis
276.736°
True anomaly
83.36341°
Mean anomaly
83.2644°
Eccentric anomaly
83.3139°
Mean motion
3.80249 °/min
Orbital period
94.67 mins
BSTAR
0.0010145
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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 | 2025-12-10 10:14:07.538Z | 204.478° SW | 2025-12-10 10:17:07.538Z | 137.008° SSE | 35.337° | 2025-12-10 10:20:07.538Z | 65.293° ENE |
| 5 mins | 2025-12-10 11:54:07.538Z | 290.177° WNW | 2025-12-10 11:56:07.538Z | 340.858° N | 25.164° | 2025-12-10 11:59:07.538Z | 32.544° NE |
| 6 mins | 2025-12-10 16:52:07.538Z | 327.543° NNW | 2025-12-10 16:54:07.538Z | 10.784° NNE | 34.104° | 2025-12-10 16:58:07.538Z | 107.247° ESE |
| 4 mins | 2025-12-10 18:31:07.538Z | 268.738° W | 2025-12-10 18:33:07.538Z | 225.322° WSW | 21.709° | 2025-12-10 18:35:07.538Z | 186.083° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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