SPACEMOBILE-003, 61045
Orbit data source: Space-Track
SPACEMOBILE-003, 61045 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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61045 intel report (Beta)
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SPACEMOBILE-003 radio frequencies
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Edit Public Description
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, 4.5 m
Radar Cross Section
1.500 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 SPACEMOBILE-003
1 61045U 24163A 25260.84553043 .00003192 00000-0 15848-3 0 9993
2 61045 52.9778 122.1075 0012158 32.4778 327.6962 15.20563103 56329Epoch: 2025-09-17T20:17Z
TLE epoch observation values (Epoch: 2025-09-17T20:17:33.829Z)
Latitude
-0°
Longitude
-179.29909°
Altitude
497.948 km
Speed
7.621 km/s
True Right ascension
08h 08m 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
04:31:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.794 km
Perigee altitude
496.058 km
Semi-major axis
6,882.563 km
Eccentricity
0.00122
Inclination
52.9778°
RAAN
122.1075°
Arg. of periapsis
32.4778°
True anomaly
327.62165°
Mean anomaly
327.6962°
Eccentric anomaly
327.65893°
Mean motion
3.80118 °/min
Orbital period
94.71 mins
BSTAR
0.00015848
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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-003 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 | 2025-09-18 16:57:20.951Z | 202.439° SSW | 2025-09-18 17:00:20.951Z | 145.879° SSE | 32.421° | 2025-09-18 17:03:20.951Z | 69.012° E |
| 5 mins | 2025-09-18 18:37:20.951Z | 284.162° WNW | 2025-09-18 18:39:20.951Z | 334.272° NNW | 26.298° | 2025-09-18 18:42:20.951Z | 31.633° NE |
| 5 mins | 2025-09-18 23:36:20.951Z | 337.938° N | 2025-09-18 23:38:20.951Z | 44.215° NE | 33.223° | 2025-09-18 23:41:20.951Z | 102.913° ESE |
| 5 mins | 2025-09-19 01:14:20.951Z | 275.57° WNW | 2025-09-19 01:16:20.951Z | 234.108° WSW | 23.436° | 2025-09-19 01:19:20.951Z | 175.842° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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