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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SPACEMOBILE-005 radio frequencies
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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, 4.5 m
Radar Cross Section
1.500 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 25260.04149635 .00004581 00000-0 22099-3 0 9993
2 61046 52.9771 125.6922 0012468 30.0110 330.1597 15.20558909 56196Epoch: 2025-09-17T00:59Z
TLE epoch observation values (Epoch: 2025-09-17T00:59:45.284Z)
Latitude
0.00002°
Longitude
114.53039°
Altitude
497.59 km
Speed
7.621 km/s
True Right ascension
08h 22m 46s
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
17:43:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.02 km
Perigee altitude
495.857 km
Semi-major axis
6,882.575 km
Eccentricity
0.00125
Inclination
52.9771°
RAAN
125.6922°
Arg. of periapsis
30.011°
True anomaly
330.08851°
Mean anomaly
330.1597°
Eccentric anomaly
330.12412°
Mean motion
3.80116 °/min
Orbital period
94.71 mins
BSTAR
0.00022099
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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 | 2025-09-18 01:10:20.625Z | 297.364° NW | 2025-09-18 01:14:20.625Z | 206.562° SW | 33.499° | 2025-09-18 01:17:20.625Z | 154.935° SSE |
| 4 mins | 2025-09-18 16:36:20.625Z | 165.264° S | 2025-09-18 16:37:20.625Z | 143.067° SSE | 22.229° | 2025-09-18 16:40:20.625Z | 80.423° E |
| 5 mins | 2025-09-18 18:14:20.625Z | 269.254° W | 2025-09-18 18:16:20.625Z | 332.843° NNW | 33.603° | 2025-09-18 18:19:20.625Z | 36.396° NE |
| 5 mins | 2025-09-18 23:13:20.625Z | 345.221° N | 2025-09-18 23:15:20.625Z | 37.408° NE | 26.037° | 2025-09-18 23:18:20.625Z | 90.463° ESE |
| 4 mins | 2025-09-19 00:51:20.625Z | 288.227° WNW | 2025-09-19 00:53:20.625Z | 242.496° WSW | 32.839° | 2025-09-19 00:55:20.625Z | 173.32° S |
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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