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 00020U 59007A 22181.36141761 .00000154 00000-0 46732-4 0 9992
2 00020 33.3573 54.6689 1665014 248.7824 92.7345 11.56229883316582
| Epoch (UTC): | 30 June 2022 08:40:26 |
| Eccentricity: | 0.1665014 |
| inclination: | 33.3573° |
| perigee height: | 507 km |
| apogee height: | 3258 km |
| right ascension of ascending node: | 54.6689° |
| argument of perigee: | 248.7824° |
| revolutions per day: | 11.56229883 |
| mean anomaly at epoch: | 92.7345° |
| orbit number at epoch: | 31658 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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