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 22182.84886763 .00000193 00000-0 55036-4 0 9991
2 35935 98.5713 40.8597 0008644 27.3182 332.8468 14.56002297677974
| Epoch (UTC): | 01 July 2022 20:22:22 |
| Eccentricity: | 0.0008644 |
| inclination: | 98.5713° |
| perigee height: | 700 km |
| apogee height: | 712 km |
| right ascension of ascending node: | 40.8597° |
| argument of perigee: | 27.3182° |
| revolutions per day: | 14.56002297 |
| mean anomaly at epoch: | 332.8468° |
| orbit number at epoch: | 67797 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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