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 25288.49987397 .00003723 00000-0 18115-3 0 9998
2 61046 52.9747 354.8671 0011937 109.7281 250.5002 15.20806704 60526Epoch: 2025-10-15T11:59Z
TLE epoch observation values (Epoch: 2025-10-15T11:59:49.111Z)
Latitude
0.00001°
Longitude
150.63942°
Altitude
507.033 km
Speed
7.61 km/s
True Right ascension
23h 39m 28s
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
15:49:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.906 km
Perigee altitude
495.476 km
Semi-major axis
6,881.828 km
Eccentricity
0.00119
Inclination
52.9747°
RAAN
354.8671°
Arg. of periapsis
109.7281°
True anomaly
250.37132°
Mean anomaly
250.5002°
Eccentric anomaly
250.43575°
Mean motion
3.80178 °/min
Orbital period
94.69 mins
BSTAR
0.00018115
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-16 07:06:00.580Z | 219.7° SW | 2025-10-16 07:09:00.580Z | 131.815° SE | 43.276° | 2025-10-16 07:12:00.580Z | 55.719° ENE |
| 4 mins | 2025-10-16 08:46:00.580Z | 297.878° NW | 2025-10-16 08:48:00.580Z | 340.157° N | 20.476° | 2025-10-16 08:50:00.580Z | 18.943° NNE |
| 6 mins | 2025-10-16 13:44:00.580Z | 318.552° NNW | 2025-10-16 13:47:00.580Z | 81.743° E | 40.031° | 2025-10-16 13:50:00.580Z | 119.796° 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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