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: 5 days ago
TLE from 5 days ago
0 SPACEMOBILE-003
1 61045U 24163A 26154.74549926 -.00039044 00000-0 -17436-2 0 9991
2 61045 52.9726 11.2534 0007638 72.5962 287.5867 15.20766851 95727Epoch: 2026-06-03T17:53Z
TLE epoch observation values (Epoch: 2026-06-03T17:53:31.136Z)
Latitude
0.00001°
Longitude
-149.32603°
Altitude
502.818 km
Speed
7.615 km/s
True Right ascension
00h 45m 00s
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
00:57:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.068 km
Perigee altitude
498.555 km
Semi-major axis
6,881.949 km
Eccentricity
0.00076
Inclination
52.9726°
RAAN
11.2534°
Arg. of periapsis
72.5962°
True anomaly
287.50324°
Mean anomaly
287.5867°
Eccentric anomaly
287.54497°
Mean motion
3.80168 °/min
Orbital period
94.69 mins
BSTAR
-0.0017436
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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 | 2026-06-08 16:25:58.473Z | 271.865° WNW | 2026-06-08 16:27:58.473Z | 329.105° NNW | 31.928° | 2026-06-08 16:30:58.473Z | 34.419° NE |
| 5 mins | 2026-06-08 21:24:58.473Z | 341.655° N | 2026-06-08 21:26:58.473Z | 34.182° NE | 27.65° | 2026-06-08 21:29:58.473Z | 92.15° ESE |
| 5 mins | 2026-06-08 23:02:58.473Z | 286.58° WNW | 2026-06-08 23:04:58.473Z | 244.957° WSW | 29.949° | 2026-06-08 23:07:58.473Z | 166.465° S |
| 4 mins | 2026-06-09 14:27:58.473Z | 170.38° S | 2026-06-09 14:28:58.473Z | 146.374° SSE | 25.22° | 2026-06-09 14:31:58.473Z | 77.891° E |
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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