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 19460U 88078A 23086.16704265 0.00000400 00000-0 14434-3 0 07
2 19460 84.9936 77.6681 0007599 62.1405 297.8594 14.33692763 02
| Epoch (UTC): | 27 March 2023 04:00:32 |
| Eccentricity: | 0.0007599 |
| inclination: | 84.9936° |
| perigee height: | 774 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 77.6681° |
| argument of perigee: | 62.1405° |
| revolutions per day: | 14.33692763 |
| mean anomaly at epoch: | 297.8594° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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