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 22028.85546212 .00007118 00000-0 13400-3 0 9995
2 25544 51.6447 306.5909 0006818 72.1061 40.7231 15.49683806323578
| Epoch (UTC): | 28 January 2022 20:31:51 |
| Eccentricity: | 0.0006818 |
| inclination: | 51.6447° |
| perigee height: | 413 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 306.5909° |
| argument of perigee: | 72.1061° |
| revolutions per day: | 15.49683806 |
| mean anomaly at epoch: | 40.7231° |
| orbit number at epoch: | 32357 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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