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 32123U 99025CRR 22182.65972112 .00000324 00000-0 72660-4 0 9998
2 32123 98.8911 248.1684 0176458 174.7332 338.4348 14.55120785530144
| Epoch (UTC): | 01 July 2022 15:49:59 |
| Eccentricity: | 0.0176458 |
| inclination: | 98.8911° |
| perigee height: | 584 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 248.1684° |
| argument of perigee: | 174.7332° |
| revolutions per day: | 14.55120785 |
| mean anomaly at epoch: | 338.4348° |
| orbit number at epoch: | 53014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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