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 43598U 98067PK 20237.30871042 +.08160231 +12416-4 +62858-3 0 9999
2 43598 051.6101 275.6733 0002578 315.8688 044.2132 16.39524565116065
| Epoch (UTC): | 24 August 2020 07:24:32 |
| Eccentricity: | 0.0002578 |
| inclination: | 51.6101° |
| perigee height: | 165 km |
| apogee height: | 169 km |
| right ascension of ascending node: | 275.6733° |
| argument of perigee: | 315.8688° |
| revolutions per day: | 16.39524565 |
| mean anomaly at epoch: | 44.2132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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