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 35296U 97051PL 22173.71221395 .00005257 00000-0 12205-2 0 9993
2 35296 86.3122 162.6762 0007727 73.1616 287.0438 14.54822315525948
| Epoch (UTC): | 22 June 2022 17:05:35 |
| Eccentricity: | 0.0007727 |
| inclination: | 86.3122° |
| perigee height: | 704 km |
| apogee height: | 715 km |
| right ascension of ascending node: | 162.6762° |
| argument of perigee: | 73.1616° |
| revolutions per day: | 14.54822315 |
| mean anomaly at epoch: | 287.0438° |
| orbit number at epoch: | 52594 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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