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 22566U 93016B 23083.95470757 -.00000132 00000-0 -43498-4 0 9990
2 22566 71.0095 324.5428 0010150 181.8449 178.2638 14.15050231549279
| Epoch (UTC): | 24 March 2023 22:54:46 |
| Eccentricity: | 0.0010150 |
| inclination: | 71.0095° |
| perigee height: | 835 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 324.5428° |
| argument of perigee: | 181.8449° |
| revolutions per day: | 14.15050231 |
| mean anomaly at epoch: | 178.2638° |
| orbit number at epoch: | 54927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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