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: 1 day ago
TLE from 1 day ago
0 SPACEMOBILE-003
1 61045U 24163A 25322.94835675 .00004733 00000-0 22512-3 0 9995
2 61045 52.9793 196.5246 0009551 200.3440 159.7175 15.20992321 65773Epoch: 2025-11-18T22:45Z
TLE epoch observation values (Epoch: 2025-11-18T22:45:38.023Z)
Latitude
-0.00002°
Longitude
156.88904°
Altitude
509.888 km
Speed
7.607 km/s
True Right ascension
13h 06m 05s
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
21:04:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.703 km
Perigee altitude
496.558 km
Semi-major axis
6,881.268 km
Eccentricity
0.00096
Inclination
52.9793°
RAAN
196.5246°
Arg. of periapsis
200.344°
True anomaly
159.7554°
Mean anomaly
159.7175°
Eccentric anomaly
159.73645°
Mean motion
3.80225 °/min
Orbital period
94.68 mins
BSTAR
0.00022512
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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 | 2025-11-20 00:28:09.763Z | 325.352° NNW | 2025-11-20 00:31:09.763Z | 34.306° NE | 33.035° | 2025-11-20 00:34:09.763Z | 100.763° ESE |
| 4 mins | 2025-11-20 02:08:09.763Z | 263.061° W | 2025-11-20 02:09:09.763Z | 239.375° WSW | 23.524° | 2025-11-20 02:12:09.763Z | 176.908° S |
| 5 mins | 2025-11-20 17:31:09.763Z | 190.3° SSW | 2025-11-20 17:33:09.763Z | 130.345° SE | 33.245° | 2025-11-20 17:36:09.763Z | 66.471° ENE |
| 4 mins | 2025-11-20 19:10:09.763Z | 290.536° WNW | 2025-11-20 19:12:09.763Z | 345.438° N | 26.016° | 2025-11-20 19:14:09.763Z | 25.241° NE |
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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