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 43547U 98067NV 21172.16341817 .12719577 12534-4 48743-3 0 9994
2 43547 51.6127 217.4511 0003370 292.8028 67.2644 16.44063265167608
| Epoch (UTC): | 21 June 2021 03:55:19 |
| Eccentricity: | 0.0003370 |
| inclination: | 51.6127° |
| perigee height: | 153 km |
| apogee height: | 157 km |
| right ascension of ascending node: | 217.4511° |
| argument of perigee: | 292.8028° |
| revolutions per day: | 16.44063265 |
| mean anomaly at epoch: | 67.2644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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