View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 58567U 23174CY 24309.97818561 .05857091 24053-5 40431-2 0 9999
2 58567 97.4081 29.7179 0009578 300.1764 59.8573 16.16392543 55554
| Epoch (UTC): | 04 November 2024 23:28:35 |
| Eccentricity: | 0.0009578 |
| inclination: | 97.4081° |
| perigee height: | 223 km |
| apogee height: | 236 km |
| right ascension of ascending node: | 29.7179° |
| argument of perigee: | 300.1764° |
| revolutions per day: | 16.16392543 |
| mean anomaly at epoch: | 59.8573° |
| orbit number at epoch: | 5555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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