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)
SPACEMOBILE-003 radio frequencies
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Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 SPACEMOBILE-003
1 61045U 24163A 25240.07620750 .00002892 00000-0 14503-3 0 9999
2 61045 52.9721 217.5835 0010454 328.8791 31.1583 15.20565609 53162
TLE epoch observation values (Epoch: 2025-08-28T01:49:44.327Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
SPACEMOBILE-003 Visibility forecast
Observer location: undefined°, undefined°
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. |
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5 mins | 2025-08-29 23:43:39.838Z | 170.705° S | 2025-08-29 23:45:39.838Z | 136.081° SSE | 18.3° | 2025-08-29 23:48:39.838Z | 82.875° E |
6 mins | 2025-08-30 01:21:39.838Z | 252.181° W | 2025-08-30 01:24:39.838Z | 348.397° N | 37.417° | 2025-08-30 01:27:39.838Z | 41.058° NE |
4 mins | 2025-08-30 06:21:39.838Z | 351.667° N | 2025-08-30 06:22:39.838Z | 14.159° NNE | 22.934° | 2025-08-30 06:25:39.838Z | 77.185° E |
6 mins | 2025-08-30 07:59:39.838Z | 294.048° NW | 2025-08-30 08:01:39.838Z | 240.408° WSW | 38.816° | 2025-08-30 08:05:39.838Z | 146.498° SSE |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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