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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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: 7 hours ago
TLE from 7 hours ago
0 SPACEMOBILE-005
1 61046U 24163B 26128.70424312 .00009047 00000-0 41895-3 0 9995
2 61046 52.9770 130.9191 0009320 6.4852 353.6261 15.20803054 91758Epoch: 2026-05-08T16:54Z
TLE epoch observation values (Epoch: 2026-05-08T16:54:06.605Z)
Latitude
-0.00005°
Longitude
10.85933°
Altitude
497.92 km
Speed
7.62 km/s
True Right ascension
08h 43m 40s
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
07:55:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.116 km
Perigee altitude
497.288 km
Semi-major axis
6,881.839 km
Eccentricity
0.00093
Inclination
52.977°
RAAN
130.9191°
Arg. of periapsis
6.4852°
True anomaly
353.61423°
Mean anomaly
353.6261°
Eccentric anomaly
353.62017°
Mean motion
3.80178 °/min
Orbital period
94.69 mins
BSTAR
0.00041895
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-09 02:31:11.365Z | 208.622° SW | 2026-05-09 02:35:11.365Z | 113.369° SE | 35.042° | 2026-05-09 02:38:11.365Z | 62.022° ENE |
| 5 mins | 2026-05-09 04:11:11.365Z | 282.613° WNW | 2026-05-09 04:13:11.365Z | 324.336° NNW | 24.454° | 2026-05-09 04:16:11.365Z | 27.149° NE |
| 5 mins | 2026-05-09 09:10:11.365Z | 330.677° NNW | 2026-05-09 09:12:11.365Z | 29.893° NE | 35.987° | 2026-05-09 09:15:11.365Z | 105.081° ESE |
| 4 mins | 2026-05-09 10:49:11.365Z | 261.55° W | 2026-05-09 10:50:11.365Z | 240.464° WSW | 20.692° | 2026-05-09 10:53:11.365Z | 182.586° 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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