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 18153U 87055B 22144.66775728 .00000425 00000-0 48794-4 0 9991
2 18153 82.5021 211.9997 0020019 264.5589 95.3342 14.83453480864472
| Epoch (UTC): | 24 May 2022 16:01:34 |
| Eccentricity: | 0.0020019 |
| inclination: | 82.5021° |
| perigee height: | 604 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 211.9997° |
| argument of perigee: | 264.5589° |
| revolutions per day: | 14.83453480 |
| mean anomaly at epoch: | 95.3342° |
| orbit number at epoch: | 86447 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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