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 36798U 10035D 24358.20995032 .00002583 00000-0 40891-3 0 9997
2 36798 97.7737 12.5528 0001599 105.8930 254.2455 14.73053227774120
| Epoch (UTC): | 23 December 2024 05:02:19 |
| Eccentricity: | 0.0001599 |
| inclination: | 97.7737° |
| perigee height: | 650 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 12.5528° |
| argument of perigee: | 105.8930° |
| revolutions per day: | 14.73053227 |
| mean anomaly at epoch: | 254.2455° |
| orbit number at epoch: | 77412 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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