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: 18 hours ago
TLE from 18 hours ago
0 SPACEMOBILE-005
1 61046U 24163B 25258.06963657 .00003931 00000-0 19185-3 0 9990
2 61046 52.9759 134.7564 0012210 23.5768 336.5783 15.20545284 55891Epoch: 2025-09-15T01:40Z
TLE epoch observation values (Epoch: 2025-09-15T01:40:16.599Z)
Latitude
-0.00006°
Longitude
115.40761°
Altitude
497.362 km
Speed
7.621 km/s
True Right ascension
08h 59m 01s
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
12:08:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.883 km
Perigee altitude
496.076 km
Semi-major axis
6,882.617 km
Eccentricity
0.00122
Inclination
52.9759°
RAAN
134.7564°
Arg. of periapsis
23.5768°
True anomaly
336.52261°
Mean anomaly
336.5783°
Eccentric anomaly
336.55046°
Mean motion
3.80113 °/min
Orbital period
94.71 mins
BSTAR
0.00019185
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-15 20:54:05.114Z | 312.04° NW | 2025-09-15 20:56:05.114Z | 344.666° N | 14.191° | 2025-09-15 20:58:05.114Z | 17.688° NNE |
| 4 mins | 2025-09-16 00:14:05.114Z | 349.004° N | 2025-09-16 00:16:05.114Z | 40.437° NE | 24.374° | 2025-09-16 00:18:05.114Z | 79.534° E |
| 5 mins | 2025-09-16 01:52:05.114Z | 290.193° WNW | 2025-09-16 01:54:05.114Z | 239.239° WSW | 35.684° | 2025-09-16 01:57:05.114Z | 156.253° SSE |
| 4 mins | 2025-09-16 17:17:05.114Z | 157.109° SSE | 2025-09-16 17:18:05.114Z | 133.985° SE | 21.336° | 2025-09-16 17:21:05.114Z | 78.354° E |
| 6 mins | 2025-09-16 18:54:05.114Z | 259.263° W | 2025-09-16 18:57:05.114Z | 349.437° N | 33.761° | 2025-09-16 19:00:05.114Z | 39.286° NE |
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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