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 43678U 18084H 22021.44406589 .00000385 00000-0 43881-4 0 9990
2 43678 97.9481 153.2390 0011146 55.0781 305.1523 14.91885492175935
| Epoch (UTC): | 21 January 2022 10:39:27 |
| Eccentricity: | 0.0011146 |
| inclination: | 97.9481° |
| perigee height: | 584 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 153.2390° |
| argument of perigee: | 55.0781° |
| revolutions per day: | 14.91885492 |
| mean anomaly at epoch: | 305.1523° |
| orbit number at epoch: | 17593 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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