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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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: 15 hours ago
TLE from 15 hours ago
0 SPACEMOBILE-005
1 61046U 24163B 26308.39911987 .00000819 00000-0 52191-4 0 9999
2 61046 52.9757 24.8934 0009817 166.5453 193.5804 15.20228611119097Epoch: 2026-11-04T09:34Z
TLE epoch observation values (Epoch: 2026-11-04T09:34:43.956Z)
Latitude
-0.00008°
Longitude
-162.4378°
Altitude
512.595 km
Speed
7.605 km/s
True Right ascension
01h 39m 34s
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
20:48:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.193 km
Perigee altitude
498.678 km
Semi-major axis
6,883.572 km
Eccentricity
0.00098
Inclination
52.9757°
RAAN
24.8934°
Arg. of periapsis
166.5453°
True anomaly
193.55402°
Mean anomaly
193.5804°
Eccentric anomaly
193.56721°
Mean motion
3.80034 °/min
Orbital period
94.73 mins
BSTAR
0.000052191
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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 | 2026-11-05 07:50:39.296Z | 224.486° SW | 2026-11-05 07:53:39.296Z | 183.429° SSW | 75.829° | 2026-11-05 07:57:39.296Z | 52.357° ENE |
| 4 mins | 2026-11-05 09:31:39.296Z | 311.484° NW | 2026-11-05 09:32:39.296Z | 332.785° NNW | 21.154° | 2026-11-05 09:35:39.296Z | 26.037° NE |
| 5 mins | 2026-11-05 14:29:39.296Z | 318.441° NNW | 2026-11-05 14:31:39.296Z | 40.735° NE | 72.276° | 2026-11-05 14:34:39.296Z | 122.046° 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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