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: 2 days ago
TLE from 2 days ago
0 SPACEMOBILE-005
1 61046U 24163B 26282.62986978 .00005469 00000-0 26180-3 0 9992
2 61046 52.9772 143.2970 0010835 92.2757 267.9478 15.20449049115172Epoch: 2026-10-09T15:07Z
TLE epoch observation values (Epoch: 2026-10-09T15:07:00.748Z)
Latitude
-0.00004°
Longitude
-101.70474°
Altitude
505.637 km
Speed
7.612 km/s
True Right ascension
09h 33m 11s
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
16:50:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.228 km
Perigee altitude
497.312 km
Semi-major axis
6,882.907 km
Eccentricity
0.00108
Inclination
52.9772°
RAAN
143.297°
Arg. of periapsis
92.2757°
True anomaly
267.82373°
Mean anomaly
267.9478°
Eccentric anomaly
267.88576°
Mean motion
3.80089 °/min
Orbital period
94.71 mins
BSTAR
0.0002618
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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 | 2026-10-11 22:47:20.161Z | 327.549° NNW | 2026-10-11 22:50:20.161Z | 22.12° NNE | 29.802° | 2026-10-11 22:53:20.161Z | 86.894° E |
| 5 mins | 2026-10-12 00:27:20.161Z | 281.315° WNW | 2026-10-12 00:29:20.161Z | 219.757° SW | 39.826° | 2026-10-12 00:32:20.161Z | 158.747° S |
| 5 mins | 2026-10-12 15:51:20.161Z | 172.949° S | 2026-10-12 15:53:20.161Z | 124.159° SE | 27.273° | 2026-10-12 15:56:20.161Z | 72.211° E |
| 5 mins | 2026-10-12 17:29:20.161Z | 268.081° W | 2026-10-12 17:31:20.161Z | 318.356° NNW | 38.826° | 2026-10-12 17:34:20.161Z | 32.515° NE |
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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