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 00020U 59007A 25193.88824206 .00000911 00000-0 37676-3 0 9994
2 00020 33.3432 47.6945 1641296 35.7636 334.2485 11.60743924445151
| Epoch (UTC): | 12 July 2025 21:19:04 |
| Eccentricity: | 0.1641296 |
| inclination: | 33.3432° |
| perigee height: | 509 km |
| apogee height: | 3214 km |
| right ascension of ascending node: | 47.6945° |
| argument of perigee: | 35.7636° |
| revolutions per day: | 11.60743924 |
| mean anomaly at epoch: | 334.2485° |
| orbit number at epoch: | 44515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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