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 22182.82264736 .00000218 00000-0 59545-4 0 9994
2 35933 98.5613 40.7806 0006313 27.4834 332.6696 14.56894538678260
| Epoch (UTC): | 01 July 2022 19:44:36 |
| Eccentricity: | 0.0006313 |
| inclination: | 98.5613° |
| perigee height: | 699 km |
| apogee height: | 707 km |
| right ascension of ascending node: | 40.7806° |
| argument of perigee: | 27.4834° |
| revolutions per day: | 14.56894538 |
| mean anomaly at epoch: | 332.6696° |
| orbit number at epoch: | 67826 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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