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 43806U 18099BA 22184.22252858 .00001005 00000-0 93121-4 0 9995
2 43806 97.6173 250.4016 0013636 207.8659 152.1834 14.96608734195119
| Epoch (UTC): | 03 July 2022 05:20:26 |
| Eccentricity: | 0.0013636 |
| inclination: | 97.6173° |
| perigee height: | 568 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 250.4016° |
| argument of perigee: | 207.8659° |
| revolutions per day: | 14.96608734 |
| mean anomaly at epoch: | 152.1834° |
| orbit number at epoch: | 19511 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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