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 42836U 17042M 23269.08812769 .00006576 00000-0 60337-3 0 9996
2 42836 97.3834 101.7237 0010517 241.8619 118.1541 14.95132929337633
| Epoch (UTC): | 26 September 2023 02:06:54 |
| Eccentricity: | 0.0010517 |
| inclination: | 97.3834° |
| perigee height: | 574 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 101.7237° |
| argument of perigee: | 241.8619° |
| revolutions per day: | 14.95132929 |
| mean anomaly at epoch: | 118.1541° |
| orbit number at epoch: | 33763 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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