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 36291U 08056G 24282.42758401 .00009463 00000-0 51301-2 0 9993
2 36291 98.4803 339.8884 0171753 30.5761 330.5285 14.05371977809663
| Epoch (UTC): | 08 October 2024 10:15:43 |
| Eccentricity: | 0.0171753 |
| inclination: | 98.4803° |
| perigee height: | 750 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 339.8884° |
| argument of perigee: | 30.5761° |
| revolutions per day: | 14.05371977 |
| mean anomaly at epoch: | 330.5285° |
| orbit number at epoch: | 80966 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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