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 25544U 98067A 22176.84895575 -.01313511 00000-0 -25961-1 0 9990
2 25544 51.6443 293.6835 0004253 293.6286 207.1694 15.49455699346527
| Epoch (UTC): | 25 June 2022 20:22:29 |
| Eccentricity: | 0.0004253 |
| inclination: | 51.6443° |
| perigee height: | 415 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 293.6835° |
| argument of perigee: | 293.6286° |
| revolutions per day: | 15.49455699 |
| mean anomaly at epoch: | 207.1694° |
| orbit number at epoch: | 34652 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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