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 19071U 88033B 23083.95164008 .00000172 00000-0 32755-3 0 9994
2 19071 90.3289 345.7872 0189809 51.8841 322.0304 13.27740297690774
| Epoch (UTC): | 24 March 2023 22:50:21 |
| Eccentricity: | 0.0189809 |
| inclination: | 90.3289° |
| perigee height: | 1012 km |
| apogee height: | 1298 km |
| right ascension of ascending node: | 345.7872° |
| argument of perigee: | 51.8841° |
| revolutions per day: | 13.27740297 |
| mean anomaly at epoch: | 322.0304° |
| orbit number at epoch: | 69077 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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