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: 10 hours ago
TLE from 10 hours ago
0 SPACEMOBILE-005
1 61046U 24163B 25299.40856830 .00004327 00000-0 20746-3 0 9992
2 61046 52.9698 304.6958 0011497 138.8259 221.3604 15.20915245 62180Epoch: 2025-10-26T09:48Z
TLE epoch observation values (Epoch: 2025-10-26T09:48:20.301Z)
Latitude
-0.00005°
Longitude
122.58599°
Altitude
509.896 km
Speed
7.607 km/s
True Right ascension
20h 18m 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
14:49:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.276 km
Perigee altitude
495.453 km
Semi-major axis
6,881.502 km
Eccentricity
0.00115
Inclination
52.9698°
RAAN
304.6958°
Arg. of periapsis
138.8259°
True anomaly
221.27344°
Mean anomaly
221.3604°
Eccentric anomaly
221.31691°
Mean motion
3.80205 °/min
Orbital period
94.69 mins
BSTAR
0.00020746
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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 | 2025-10-27 03:21:21.282Z | 234.261° WSW | 2025-10-27 03:23:21.282Z | 293.451° NW | 44.702° | 2025-10-27 03:26:21.282Z | 48.203° ENE |
| 4 mins | 2025-10-27 08:20:21.282Z | 349.057° N | 2025-10-27 08:22:21.282Z | 29.525° NE | 18.248° | 2025-10-27 08:24:21.282Z | 64.544° ENE |
| 6 mins | 2025-10-27 09:58:21.282Z | 309.524° NW | 2025-10-27 10:01:21.282Z | 132.53° SE | 43.445° | 2025-10-27 10:04:21.282Z | 131.048° SE |
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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