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 25321.27955887 .00003548 00000-0 14240-2 0 9990
2 00020 33.3451 309.7598 1639586 357.7381 1.6456 11.61481611459961
| Epoch (UTC): | 17 November 2025 06:42:33 |
| Eccentricity: | 0.1639586 |
| inclination: | 33.3451° |
| perigee height: | 507 km |
| apogee height: | 3208 km |
| right ascension of ascending node: | 309.7598° |
| argument of perigee: | 357.7381° |
| revolutions per day: | 11.61481611 |
| mean anomaly at epoch: | 1.6456° |
| orbit number at epoch: | 45996 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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