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 35933U 09051C 22175.81734638 .00000392 00000-0 98185-4 0 9994
2 35933 98.5623 33.5854 0006670 46.1666 314.0082 14.56889169677245
| Epoch (UTC): | 24 June 2022 19:36:58 |
| Eccentricity: | 0.0006670 |
| inclination: | 98.5623° |
| perigee height: | 698 km |
| apogee height: | 708 km |
| right ascension of ascending node: | 33.5854° |
| argument of perigee: | 46.1666° |
| revolutions per day: | 14.56889169 |
| mean anomaly at epoch: | 314.0082° |
| orbit number at epoch: | 67724 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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