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 25411U 98045E 24358.22162723 .00000178 00000-0 20995-3 0 9990
2 25411 70.9872 32.0050 0209917 155.9417 205.1666 13.71186640320871
| Epoch (UTC): | 23 December 2024 05:19:08 |
| Eccentricity: | 0.0209917 |
| inclination: | 70.9872° |
| perigee height: | 840 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 32.0050° |
| argument of perigee: | 155.9417° |
| revolutions per day: | 13.71186640 |
| mean anomaly at epoch: | 205.1666° |
| orbit number at epoch: | 32087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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