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 21796U 91081A 23088.76393890 .00000104 00000-0 91425-4 0 9990
2 21796 82.9559 320.9302 0049900 26.9992 16.4168 13.75578117572794
| Epoch (UTC): | 29 March 2023 18:20:04 |
| Eccentricity: | 0.0049900 |
| inclination: | 82.9559° |
| perigee height: | 943 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 320.9302° |
| argument of perigee: | 26.9992° |
| revolutions per day: | 13.75578117 |
| mean anomaly at epoch: | 16.4168° |
| orbit number at epoch: | 57279 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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