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 25257.08370546 .00003857 00000-0 18841-3 0 9995
2 61046 52.9750 139.2878 0012120 19.7995 340.3468 15.20559549 55745Epoch: 2025-09-14T02:00Z
TLE epoch observation values (Epoch: 2025-09-14T02:00:32.151Z)
Latitude
0.00002°
Longitude
115.84606°
Altitude
497.174 km
Speed
7.622 km/s
True Right ascension
09h 17m 09s
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
02:56:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.779 km
Perigee altitude
496.095 km
Semi-major axis
6,882.574 km
Eccentricity
0.00121
Inclination
52.975°
RAAN
139.2878°
Arg. of periapsis
19.7995°
True anomaly
340.30002°
Mean anomaly
340.3468°
Eccentric anomaly
340.32342°
Mean motion
3.80117 °/min
Orbital period
94.71 mins
BSTAR
0.00018841
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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 | 2025-09-15 17:35:52.336Z | 177.285° S | 2025-09-15 17:38:52.336Z | 118.745° SE | 20.323° | 2025-09-15 17:40:52.336Z | 83.161° E |
| 5 mins | 2025-09-15 19:14:52.336Z | 264.529° W | 2025-09-15 19:16:52.336Z | 331.488° NNW | 35.674° | 2025-09-15 19:19:52.336Z | 37.735° NE |
| 5 mins | 2025-09-16 00:13:52.336Z | 345.934° N | 2025-09-16 00:15:52.336Z | 35.431° NE | 24.692° | 2025-09-16 00:18:52.336Z | 87.611° E |
| 6 mins | 2025-09-16 01:51:52.336Z | 291.776° WNW | 2025-09-16 01:53:52.336Z | 247.855° W | 34.972° | 2025-09-16 01:57:52.336Z | 151.733° SSE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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