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 is defined by the following mean orbital elements,
1 42765U 17036A 23323.04012457 .14030009 24427-5 36327-3 0 9992
2 42765 97.0925 4.4532 0009179 243.7660 116.2700 16.45229930358149
| Epoch (UTC): | 19 November 2023 00:57:46 |
| Eccentricity: | 0.0009179 |
| inclination: | 97.0925° |
| perigee height: | 146 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 4.4532° |
| argument of perigee: | 243.7660° |
| revolutions per day: | 16.45229930 |
| mean anomaly at epoch: | 116.2700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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