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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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-003
1 61045U 24163A 26249.51535588 -.00000656 00000-0 -14902-4 0 9994
2 61045 52.9686 295.4918 0004987 13.6324 346.4803 15.20492433110147Epoch: 2026-09-06T12:22Z
TLE epoch observation values (Epoch: 2026-09-06T12:22:06.748Z)
Latitude
-0.00007°
Longitude
124.35427°
Altitude
501.893 km
Speed
7.616 km/s
True Right ascension
19h 41m 58s
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
11:37:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.073 km
Perigee altitude
501.208 km
Semi-major axis
6,882.777 km
Eccentricity
0.0005
Inclination
52.9686°
RAAN
295.4918°
Arg. of periapsis
13.6324°
True anomaly
346.46693°
Mean anomaly
346.4803°
Eccentric anomaly
346.47362°
Mean motion
3.801 °/min
Orbital period
94.71 mins
BSTAR
-0.000014902
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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 | 2026-09-09 05:14:51.574Z | 231.303° WSW | 2026-09-09 05:16:51.574Z | 277.644° WNW | 86.038° | 2026-09-09 05:19:51.574Z | 49.361° ENE |
| 4 mins | 2026-09-09 10:13:51.574Z | 348.184° N | 2026-09-09 10:15:51.574Z | 27.163° NE | 19.121° | 2026-09-09 10:17:51.574Z | 62.071° ENE |
| 6 mins | 2026-09-09 11:51:51.574Z | 311.478° NW | 2026-09-09 11:54:51.574Z | 105.173° ESE | 77.533° | 2026-09-09 11:57:51.574Z | 128.399° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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