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 00020U 59007A 23087.62120636 .00004153 00000-0 16719-2 0 9998
2 00020 33.3524 167.0901 1659823 249.6069 91.9014 11.57172738347996
| Epoch (UTC): | 28 March 2023 14:54:32 |
| Eccentricity: | 0.1659823 |
| inclination: | 33.3524° |
| perigee height: | 508 km |
| apogee height: | 3249 km |
| right ascension of ascending node: | 167.0901° |
| argument of perigee: | 249.6069° |
| revolutions per day: | 11.57172738 |
| mean anomaly at epoch: | 91.9014° |
| orbit number at epoch: | 34799 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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