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 22144.28804957 .00010966 00000-0 20228-3 0 9995
2 25544 51.6435 94.9540 0005191 152.1188 357.1533 15.49646925341476
| Epoch (UTC): | 24 May 2022 06:54:47 |
| Eccentricity: | 0.0005191 |
| inclination: | 51.6435° |
| perigee height: | 414 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 94.9540° |
| argument of perigee: | 152.1188° |
| revolutions per day: | 15.49646925 |
| mean anomaly at epoch: | 357.1533° |
| orbit number at epoch: | 34147 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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