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: 21 hours ago
TLE from 21 hours ago
0 SPACEMOBILE-005
1 61046U 24163B 26062.33922177 .00012981 00000-0 58819-3 0 9998
2 61046 52.9771 76.1973 0011318 161.3309 198.8103 15.21148833 81656Epoch: 2026-03-03T08:08Z
TLE epoch observation values (Epoch: 2026-03-03T08:08:28.760Z)
Latitude
-0.00002°
Longitude
152.95775°
Altitude
510.623 km
Speed
7.606 km/s
True Right ascension
05h 04m 47s
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
08:45:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.447 km
Perigee altitude
494.871 km
Semi-major axis
6,880.796 km
Eccentricity
0.00113
Inclination
52.9771°
RAAN
76.1973°
Arg. of periapsis
161.3309°
True anomaly
198.76854°
Mean anomaly
198.8103°
Eccentric anomaly
198.78941°
Mean motion
3.80264 °/min
Orbital period
94.67 mins
BSTAR
0.00058819
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-04 09:52:14.497Z | 325.388° NNW | 2026-03-04 09:54:14.497Z | 20.702° NNE | 38.509° | 2026-03-04 09:57:14.497Z | 110.021° ESE |
| 4 mins | 2026-03-04 11:31:14.497Z | 260.071° W | 2026-03-04 11:32:14.497Z | 240.964° WSW | 17.481° | 2026-03-04 11:35:14.497Z | 187.504° SSW |
| 5 mins | 2026-03-05 02:54:14.497Z | 206.642° SW | 2026-03-05 02:56:14.497Z | 133.903° SE | 40.39° | 2026-03-05 02:59:14.497Z | 59.711° ENE |
| 4 mins | 2026-03-05 04:33:14.497Z | 295.44° NW | 2026-03-05 04:35:14.497Z | 341.207° N | 22.378° | 2026-03-05 04:37:14.497Z | 20.727° NNE |
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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