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 23036.86457072 .00003020 00000-0 12407-2 0 9997
2 00020 33.3500 348.2913 1660238 339.7258 14.4280 11.56682152342118
| Epoch (UTC): | 05 February 2023 20:44:58 |
| Eccentricity: | 0.1660238 |
| inclination: | 33.3500° |
| perigee height: | 509 km |
| apogee height: | 3252 km |
| right ascension of ascending node: | 348.2913° |
| argument of perigee: | 339.7258° |
| revolutions per day: | 11.56682152 |
| mean anomaly at epoch: | 14.4280° |
| orbit number at epoch: | 34211 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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