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 43192U 18015A 23075.16838495 .09853696 25597-5 22543-2 0 9992
2 43192 97.5320 239.1494 0008581 277.2576 207.7039 16.29975082285605
| Epoch (UTC): | 16 March 2023 04:02:28 |
| Eccentricity: | 0.0008581 |
| inclination: | 97.5320° |
| perigee height: | 187 km |
| apogee height: | 198 km |
| right ascension of ascending node: | 239.1494° |
| argument of perigee: | 277.2576° |
| revolutions per day: | 16.29975082 |
| mean anomaly at epoch: | 207.7039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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