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 22177.55731902 .00000346 00000-0 89588-4 0 9996
2 35935 98.5722 35.4262 0008922 41.9806 318.2073 14.55999021677202
| Epoch (UTC): | 26 June 2022 13:22:32 |
| Eccentricity: | 0.0008922 |
| inclination: | 98.5722° |
| perigee height: | 700 km |
| apogee height: | 712 km |
| right ascension of ascending node: | 35.4262° |
| argument of perigee: | 41.9806° |
| revolutions per day: | 14.55999021 |
| mean anomaly at epoch: | 318.2073° |
| orbit number at epoch: | 67720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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