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: 15 hours ago
TLE from 15 hours ago
0 SPACEMOBILE-005
1 61046U 24163B 26106.75704541 -.00001171 00000-0 -37276-4 0 9992
2 61046 52.9773 231.8556 0008808 308.8116 51.2091 15.21110613 88413Epoch: 2026-04-16T18:10Z
TLE epoch observation values (Epoch: 2026-04-16T18:10:08.723Z)
Latitude
-0.00005°
Longitude
114.41921°
Altitude
499.573 km
Speed
7.618 km/s
True Right ascension
15h 27m 25s
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
15:58:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.835 km
Perigee altitude
496.714 km
Semi-major axis
6,880.911 km
Eccentricity
0.00088
Inclination
52.9773°
RAAN
231.8556°
Arg. of periapsis
308.8116°
True anomaly
51.28782°
Mean anomaly
51.2091°
Eccentric anomaly
51.24846°
Mean motion
3.80254 °/min
Orbital period
94.67 mins
BSTAR
-0.000037276
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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 | 2026-04-17 10:05:28.624Z | 180.506° SSW | 2026-04-17 10:08:28.624Z | 120.731° SE | 22.092° | 2026-04-17 10:10:28.624Z | 82.942° E |
| 5 mins | 2026-04-17 11:44:28.624Z | 266.397° W | 2026-04-17 11:46:28.624Z | 326.993° NNW | 34.535° | 2026-04-17 11:49:28.624Z | 36.019° NE |
| 5 mins | 2026-04-17 16:43:28.624Z | 344.846° N | 2026-04-17 16:45:28.624Z | 35.5° NE | 25.827° | 2026-04-17 16:48:28.624Z | 89.163° E |
| 6 mins | 2026-04-17 18:21:28.624Z | 289.483° WNW | 2026-04-17 18:23:28.624Z | 244.596° WSW | 33.613° | 2026-04-17 18:27:28.624Z | 154.032° SSE |
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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