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 23026.32746090 .00003356 00000-0 13661-2 0 9993
2 00020 33.3579 25.8766 1660909 283.7579 58.4203 11.56624775340890
| Epoch (UTC): | 26 January 2023 07:51:32 |
| Eccentricity: | 0.1660909 |
| inclination: | 33.3579° |
| perigee height: | 509 km |
| apogee height: | 3253 km |
| right ascension of ascending node: | 25.8766° |
| argument of perigee: | 283.7579° |
| revolutions per day: | 11.56624775 |
| mean anomaly at epoch: | 58.4203° |
| orbit number at epoch: | 34089 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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