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: 1 day ago
TLE from 1 day ago
0 SPACEMOBILE-005
1 61046U 24163B 26259.35967635 .00009452 00000-0 44248-3 0 9996
2 61046 52.9722 250.2353 0009404 32.8814 327.2764 15.20372408111634Epoch: 2026-09-16T08:37Z
TLE epoch observation values (Epoch: 2026-09-16T08:37:56.036Z)
Latitude
0.00002°
Longitude
125.43944°
Altitude
500.149 km
Speed
7.619 km/s
True Right ascension
16h 40m 56s
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
03:02:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.475 km
Perigee altitude
498.529 km
Semi-major axis
6,883.139 km
Eccentricity
0.00094
Inclination
52.9722°
RAAN
250.2353°
Arg. of periapsis
32.8814°
True anomaly
327.21809°
Mean anomaly
327.2764°
Eccentric anomaly
327.24725°
Mean motion
3.8007 °/min
Orbital period
94.72 mins
BSTAR
0.00044248
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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 | 2026-09-18 01:50:26.663Z | 225.18° WSW | 2026-09-18 01:52:26.663Z | 209.729° SW | 68.741° | 2026-09-18 01:56:26.663Z | 51.839° ENE |
| 4 mins | 2026-09-18 03:30:26.663Z | 308.355° NW | 2026-09-18 03:31:26.663Z | 328.575° NNW | 20.217° | 2026-09-18 03:34:26.663Z | 23.808° NE |
| 6 mins | 2026-09-18 08:28:26.663Z | 316.487° NNW | 2026-09-18 08:30:26.663Z | 15.212° NNE | 73.835° | 2026-09-18 08:34:26.663Z | 124.863° 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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