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 23336.42774584 .00001683 00000-0 68153-3 0 9995
2 00020 33.3452 357.6889 1656407 133.9008 241.0870 11.57987419376834
| Epoch (UTC): | 02 December 2023 10:15:57 |
| Eccentricity: | 0.1656407 |
| inclination: | 33.3452° |
| perigee height: | 507 km |
| apogee height: | 3241 km |
| right ascension of ascending node: | 357.6889° |
| argument of perigee: | 133.9008° |
| revolutions per day: | 11.57987419 |
| mean anomaly at epoch: | 241.0870° |
| orbit number at epoch: | 37683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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