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 19210U 88050A 24281.37252021 .00020696 00000-0 10172-2 0 9999
2 19210 82.5118 315.7762 0015618 139.1633 221.0774 15.17817953958864
| Epoch (UTC): | 07 October 2024 08:56:25 |
| Eccentricity: | 0.0015618 |
| inclination: | 82.5118° |
| perigee height: | 501 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 315.7762° |
| argument of perigee: | 139.1633° |
| revolutions per day: | 15.17817953 |
| mean anomaly at epoch: | 221.0774° |
| orbit number at epoch: | 95886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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