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 35635U 09039A 23083.46048765 .00000321 00000-0 24829-3 0 9993
2 35635 82.9594 202.3517 0020031 40.9261 29.9814 13.89724607693399
| Epoch (UTC): | 24 March 2023 11:03:06 |
| Eccentricity: | 0.0020031 |
| inclination: | 82.9594° |
| perigee height: | 915 km |
| apogee height: | 944 km |
| right ascension of ascending node: | 202.3517° |
| argument of perigee: | 40.9261° |
| revolutions per day: | 13.89724607 |
| mean anomaly at epoch: | 29.9814° |
| orbit number at epoch: | 69339 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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