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 20U 59007A 23036.17357130 .00002868 00000-0 11772-2 0 9998
2 20 33.3507 350.7567 1660276 336.0529 17.0740 11.56677668342061
| Epoch (UTC): | 05 February 2023 04:09:56 |
| Eccentricity: | 0.1660276 |
| inclination: | 33.3507° |
| perigee height: | 509 km |
| apogee height: | 3252 km |
| right ascension of ascending node: | 350.7567° |
| argument of perigee: | 336.0529° |
| revolutions per day: | 11.56677668 |
| mean anomaly at epoch: | 17.0740° |
| orbit number at epoch: | 34206 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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