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 42765U 17036A 23270.66826387 .00164577 00000-0 14185-2 0 9992
2 42765 97.1279 309.9080 0004830 90.4967 269.6849 15.68751776349250
| Epoch (UTC): | 27 September 2023 16:02:17 |
| Eccentricity: | 0.0004830 |
| inclination: | 97.1279° |
| perigee height: | 359 km |
| apogee height: | 366 km |
| right ascension of ascending node: | 309.9080° |
| argument of perigee: | 90.4967° |
| revolutions per day: | 15.68751776 |
| mean anomaly at epoch: | 269.6849° |
| orbit number at epoch: | 34925 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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