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 33499U 09002H 22136.17697685 .00000951 00000-0 14598-3 0 9997
2 33499 98.2222 17.6813 0010286 62.4075 297.8178 14.75959909715915
| Epoch (UTC): | 16 May 2022 04:14:50 |
| Eccentricity: | 0.0010286 |
| inclination: | 98.2222° |
| perigee height: | 635 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 17.6813° |
| argument of perigee: | 62.4075° |
| revolutions per day: | 14.75959909 |
| mean anomaly at epoch: | 297.8178° |
| orbit number at epoch: | 71591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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