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: 5 hours ago
TLE from 5 hours ago
0 SPACEMOBILE-003
1 61045U 24163A 25343.51584833 .00027253 00000-0 12276-2 0 9995
2 61045 52.9725 101.9303 0007944 269.8727 90.1357 15.20862514 68902Epoch: 2025-12-09T12:22Z
TLE epoch observation values (Epoch: 2025-12-09T12:22:49.295Z)
Latitude
-0.00003°
Longitude
-162.27453°
Altitude
504.131 km
Speed
7.613 km/s
True Right ascension
06h 47m 43s
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
15:17:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.99 km
Perigee altitude
498.056 km
Semi-major axis
6,881.66 km
Eccentricity
0.00079
Inclination
52.9725°
RAAN
101.9303°
Arg. of periapsis
269.8727°
True anomaly
90.22673°
Mean anomaly
90.1357°
Eccentric anomaly
90.18122°
Mean motion
3.80192 °/min
Orbital period
94.69 mins
BSTAR
0.0012276
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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 | 2025-12-09 17:36:28.483Z | 315.645° NNW | 2025-12-09 17:39:28.483Z | 40.725° NE | 43.058° | 2025-12-09 17:42:28.483Z | 120.231° SE |
| 5 mins | 2025-12-10 10:39:28.483Z | 219.892° SW | 2025-12-10 10:41:28.483Z | 109.695° ESE | 44.011° | 2025-12-10 10:44:28.483Z | 53.795° ENE |
| 4 mins | 2025-12-10 12:18:28.483Z | 300.616° NW | 2025-12-10 12:20:28.483Z | 342.213° N | 20.074° | 2025-12-10 12:22:28.483Z | 19.494° NNE |
| 4 mins | 2025-12-10 15:38:28.483Z | 353.792° N | 2025-12-10 15:39:28.483Z | 12.475° NNE | 16.845° | 2025-12-10 15:42:28.483Z | 63.218° ENE |
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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