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 33899U 93036DC 24357.56622991 .00007069 00000-0 15301-2 0 9998
2 33899 74.0559 41.9866 0062048 198.7969 311.9484 14.57189353836583
| Epoch (UTC): | 22 December 2024 13:35:22 |
| Eccentricity: | 0.0062048 |
| inclination: | 74.0559° |
| perigee height: | 658 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 41.9866° |
| argument of perigee: | 198.7969° |
| revolutions per day: | 14.57189353 |
| mean anomaly at epoch: | 311.9484° |
| orbit number at epoch: | 83658 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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