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 22565U 93016A 23151.71115521 .00000075 00000-0 67157-4 0 9996
2 22565 70.8148 142.9285 0004610 147.1235 213.0172 14.12424732556535
| Epoch (UTC): | 31 May 2023 17:04:03 |
| Eccentricity: | 0.0004610 |
| inclination: | 70.8148° |
| perigee height: | 848 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 142.9285° |
| argument of perigee: | 147.1235° |
| revolutions per day: | 14.12424732 |
| mean anomaly at epoch: | 213.0172° |
| orbit number at epoch: | 55653 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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