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 35606U 93036AMZ 22222.19841346 .00000376 00000-0 40263-3 0 9991
2 35606 73.8094 150.4170 0464880 186.1829 173.3413 13.38058813446967
| Epoch (UTC): | 10 August 2022 04:45:42 |
| Eccentricity: | 0.0464880 |
| inclination: | 73.8094° |
| perigee height: | 768 km |
| apogee height: | 1465 km |
| right ascension of ascending node: | 150.4170° |
| argument of perigee: | 186.1829° |
| revolutions per day: | 13.38058813 |
| mean anomaly at epoch: | 173.3413° |
| orbit number at epoch: | 44696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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