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 42768U 17036D 23083.12097006 .00989670 43589-3 27993-2 0 9998
2 42768 97.1491 131.9355 0004246 258.4823 101.5976 15.93489692320522
| Epoch (UTC): | 24 March 2023 02:54:11 |
| Eccentricity: | 0.0004246 |
| inclination: | 97.1491° |
| perigee height: | 290 km |
| apogee height: | 295 km |
| right ascension of ascending node: | 131.9355° |
| argument of perigee: | 258.4823° |
| revolutions per day: | 15.93489692 |
| mean anomaly at epoch: | 101.5976° |
| orbit number at epoch: | 32052 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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