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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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, 6.5 m
Radar Cross Section
32.590 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 SPACEMOBILE-003
1 61045U 24163A 26009.13700419 .00011698 00000-0 53320-3 0 9995
2 61045 52.9778 321.0754 0010026 20.8684 339.2718 15.21058290 73562Epoch: 2026-01-09T03:17Z
TLE epoch observation values (Epoch: 2026-01-09T03:17:17.162Z)
Latitude
0.00002°
Longitude
163.07283°
Altitude
497.073 km
Speed
7.621 km/s
True Right ascension
21h 24m 18s
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
13:34:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.831 km
Perigee altitude
496.033 km
Semi-major axis
6,881.069 km
Eccentricity
0.001
Inclination
52.9778°
RAAN
321.0754°
Arg. of periapsis
20.8684°
True anomaly
339.23109°
Mean anomaly
339.2718°
Eccentric anomaly
339.25145°
Mean motion
3.80241 °/min
Orbital period
94.68 mins
BSTAR
0.0005332
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-01-09 22:21:42.402Z | 179.762° S | 2026-01-09 22:24:42.402Z | 122.537° SE | 21.01° | 2026-01-09 22:26:42.402Z | 84.644° E |
| 5 mins | 2026-01-10 00:00:42.402Z | 263.826° W | 2026-01-10 00:02:42.402Z | 324.36° NNW | 35.263° | 2026-01-10 00:05:42.402Z | 36.513° NE |
| 5 mins | 2026-01-10 04:59:42.402Z | 345.094° N | 2026-01-10 05:01:42.402Z | 34.569° NE | 24.975° | 2026-01-10 05:04:42.402Z | 87.843° E |
| 6 mins | 2026-01-10 06:37:42.402Z | 291.157° WNW | 2026-01-10 06:39:42.402Z | 247.067° WSW | 34.486° | 2026-01-10 06:43:42.402Z | 152.434° 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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