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 43477U 18047B 22027.16782405 +.00000079 00000-0 +32065-5 0 01
2 43477 88.9805 57.6791 0018063 163.2388 294.1557 15.24408624204891
| Epoch (UTC): | 27 January 2022 04:01:39 |
| Eccentricity: | 0.0018063 |
| inclination: | 88.9805° |
| perigee height: | 480 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 57.6791° |
| argument of perigee: | 163.2388° |
| revolutions per day: | 15.24408624 |
| mean anomaly at epoch: | 294.1557° |
| orbit number at epoch: | 20489 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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