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 35935U 09051E 23087.54715017 .00001536 00000-0 35623-3 0 9997
2 35935 98.5364 317.3330 0006819 273.3492 86.6925 14.56504433717259
| Epoch (UTC): | 28 March 2023 13:07:53 |
| Eccentricity: | 0.0006819 |
| inclination: | 98.5364° |
| perigee height: | 699 km |
| apogee height: | 709 km |
| right ascension of ascending node: | 317.3330° |
| argument of perigee: | 273.3492° |
| revolutions per day: | 14.56504433 |
| mean anomaly at epoch: | 86.6925° |
| orbit number at epoch: | 71725 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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