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 22229.51637829 .00005615 00000-0 10551-3 0 9990
2 25544 51.6423 32.7582 0005546 131.0950 333.6691 15.50210737354698
| Epoch (UTC): | 17 August 2022 12:23:35 |
| Eccentricity: | 0.0005546 |
| inclination: | 51.6423° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 32.7582° |
| argument of perigee: | 131.0950° |
| revolutions per day: | 15.50210737 |
| mean anomaly at epoch: | 333.6691° |
| orbit number at epoch: | 35469 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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