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: 13 hours ago
TLE from 13 hours ago
0 SPACEMOBILE-005
1 61046U 24163B 26238.45755000 .00013014 00000-0 59990-3 0 9994
2 61046 52.9837 346.3033 0007965 336.4687 23.5942 15.20581042108450Epoch: 2026-08-26T10:58Z
TLE epoch observation values (Epoch: 2026-08-26T10:58:52.320Z)
Latitude
-0.00003°
Longitude
-153.12499°
Altitude
499.941 km
Speed
7.618 km/s
True Right ascension
23h 05m 12s
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
14:57:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.853 km
Perigee altitude
498.889 km
Semi-major axis
6,882.508 km
Eccentricity
0.0008
Inclination
52.9837°
RAAN
346.3033°
Arg. of periapsis
336.4687°
True anomaly
23.63077°
Mean anomaly
23.5942°
Eccentric anomaly
23.61248°
Mean motion
3.80122 °/min
Orbital period
94.71 mins
BSTAR
0.0005999
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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 | 2026-08-27 09:13:00.860Z | 196.164° SSW | 2026-08-27 09:16:00.860Z | 141.243° SSE | 28.622° | 2026-08-27 09:19:00.860Z | 72.746° E |
| 5 mins | 2026-08-27 10:53:00.860Z | 280.514° WNW | 2026-08-27 10:55:00.860Z | 336.981° NNW | 29.014° | 2026-08-27 10:58:00.860Z | 33.89° NE |
| 5 mins | 2026-08-27 15:52:00.860Z | 342.59° N | 2026-08-27 15:54:00.860Z | 43.698° NE | 30.184° | 2026-08-27 15:57:00.860Z | 98.197° ESE |
| 5 mins | 2026-08-27 17:30:00.860Z | 279.348° WNW | 2026-08-27 17:32:00.860Z | 234.112° WSW | 27.231° | 2026-08-27 17:35:00.860Z | 170.053° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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