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: 9 hours ago
TLE from 9 hours ago
0 SPACEMOBILE-005
1 61046U 24163B 26038.62016458 .00026070 00000-0 11646-2 0 9999
2 61046 52.9807 185.3075 0012799 91.9001 268.3460 15.21127892 78043Epoch: 2026-02-07T14:53Z
TLE epoch observation values (Epoch: 2026-02-07T14:53:02.219Z)
Latitude
0.00001°
Longitude
-175.69281°
Altitude
503.58 km
Speed
7.614 km/s
True Right ascension
12h 21m 13s
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
02:09:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.528 km
Perigee altitude
493.915 km
Semi-major axis
6,880.859 km
Eccentricity
0.00128
Inclination
52.9807°
RAAN
185.3075°
Arg. of periapsis
91.9001°
True anomaly
268.1994°
Mean anomaly
268.346°
Eccentric anomaly
268.2727°
Mean motion
3.80259 °/min
Orbital period
94.67 mins
BSTAR
0.0011646
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-08 11:32:44.800Z | 183.49° SSW | 2026-02-08 11:34:44.800Z | 142.551° SSE | 25.406° | 2026-02-08 11:37:44.800Z | 76.443° E |
| 5 mins | 2026-02-08 13:11:44.800Z | 275.921° WNW | 2026-02-08 13:13:44.800Z | 336.593° NNW | 30.871° | 2026-02-08 13:16:44.800Z | 35.237° NE |
| 4 mins | 2026-02-08 18:10:44.800Z | 347.348° N | 2026-02-08 18:12:44.800Z | 46.571° ENE | 27.204° | 2026-02-08 18:14:44.800Z | 87.147° E |
| 5 mins | 2026-02-08 19:48:44.800Z | 280.757° WNW | 2026-02-08 19:50:44.800Z | 228.509° WSW | 29.912° | 2026-02-08 19:53:44.800Z | 163.944° S |
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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