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: 6 days ago
TLE from 6 days ago
0 SPACEMOBILE-005
1 61046U 24163B 26153.80939865 .00006410 00000-0 30135-3 0 9994
2 61046 52.9732 15.4892 0010438 77.4279 282.7882 15.20784040 95572Epoch: 2026-06-02T19:25Z
TLE epoch observation values (Epoch: 2026-06-02T19:25:32.043Z)
Latitude
-0.00002°
Longitude
-167.17137°
Altitude
502.768 km
Speed
7.615 km/s
True Right ascension
01h 01m 57s
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
02:21:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.943 km
Perigee altitude
496.577 km
Semi-major axis
6,881.897 km
Eccentricity
0.00104
Inclination
52.9732°
RAAN
15.4892°
Arg. of periapsis
77.4279°
True anomaly
282.67152°
Mean anomaly
282.7882°
Eccentric anomaly
282.72986°
Mean motion
3.80173 °/min
Orbital period
94.69 mins
BSTAR
0.00030135
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-08 17:39:31.291Z | 304.684° NW | 2026-06-08 17:41:31.291Z | 337.824° N | 15.56° | 2026-06-08 17:43:31.291Z | 13.683° NNE |
| 4 mins | 2026-06-08 20:59:31.291Z | 347.034° N | 2026-06-08 21:01:31.291Z | 31.014° NE | 21.138° | 2026-06-08 21:03:31.291Z | 69.897° E |
| 6 mins | 2026-06-08 22:37:31.291Z | 300.87° NW | 2026-06-08 22:40:31.291Z | 184.324° SSW | 40.494° | 2026-06-08 22:43:31.291Z | 142.011° SSE |
| 6 mins | 2026-06-09 15:39:31.291Z | 247.732° W | 2026-06-09 15:42:31.291Z | 356.606° N | 38.986° | 2026-06-09 15:45:31.291Z | 43.13° 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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