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 26193.37078742 .00003105 00000-0 15376-3 0 9996
2 61046 52.9783 193.5770 0008681 187.3412 172.7457 15.20767447101596Epoch: 2026-07-12T08:53Z
TLE epoch observation values (Epoch: 2026-07-12T08:53:56.033Z)
Latitude
0.00004°
Longitude
129.82294°
Altitude
510.327 km
Speed
7.607 km/s
True Right ascension
12h 54m 18s
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
09:59:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.783 km
Perigee altitude
497.835 km
Semi-major axis
6,881.946 km
Eccentricity
0.00087
Inclination
52.9783°
RAAN
193.577°
Arg. of periapsis
187.3412°
True anomaly
172.75825°
Mean anomaly
172.7457°
Eccentric anomaly
172.75198°
Mean motion
3.80169 °/min
Orbital period
94.69 mins
BSTAR
0.00015376
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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 | 2026-07-13 02:25:03.749Z | 209.14° SW | 2026-07-13 02:28:03.749Z | 132.42° SE | 38.486° | 2026-07-13 02:31:03.749Z | 61.715° ENE |
| 4 mins | 2026-07-13 04:05:03.749Z | 293.797° NW | 2026-07-13 04:07:03.749Z | 341.581° N | 23.474° | 2026-07-13 04:09:03.749Z | 21.622° NNE |
| 6 mins | 2026-07-13 09:03:03.749Z | 324.641° NNW | 2026-07-13 09:05:03.749Z | 6.555° NNE | 36.131° | 2026-07-13 09:09:03.749Z | 111.364° ESE |
| 4 mins | 2026-07-13 10:42:03.749Z | 266.261° W | 2026-07-13 10:44:03.749Z | 226.116° WSW | 18.944° | 2026-07-13 10:46:03.749Z | 189.783° SSW |
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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