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 is defined by the following mean orbital elements,
1 43591U 98067PF 20323.57107911 +.11695971 +12499-4 +37838-3 0 9993
2 43591 051.6155 198.6835 0005882 255.3071 104.7305 16.44501217130390
| Epoch (UTC): | 18 November 2020 13:42:21 |
| Eccentricity: | 0.0005882 |
| inclination: | 51.6155° |
| perigee height: | 150 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 198.6835° |
| argument of perigee: | 255.3071° |
| revolutions per day: | 16.44501217 |
| mean anomaly at epoch: | 104.7305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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