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 00022U 59009A 22274.86573354 .00003355 00000-0 25857-3 0 9991
2 00022 50.2817 133.0045 0133637 218.2285 140.9129 14.97492821595570
| Epoch (UTC): | 01 October 2022 20:46:39 |
| Eccentricity: | 0.0133637 |
| inclination: | 50.2817° |
| perigee height: | 482 km |
| apogee height: | 667 km |
| right ascension of ascending node: | 133.0045° |
| argument of perigee: | 218.2285° |
| revolutions per day: | 14.97492821 |
| mean anomaly at epoch: | 140.9129° |
| orbit number at epoch: | 59557 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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