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 26621U 00075C 23088.84641990 -.00000846 00000-0 -75965-3 0 9996
2 26621 95.4007 215.7528 0712603 40.2691 324.9033 13.04347947 63550
| Epoch (UTC): | 29 March 2023 20:18:50 |
| Eccentricity: | 0.0712603 |
| inclination: | 95.4007° |
| perigee height: | 702 km |
| apogee height: | 1788 km |
| right ascension of ascending node: | 215.7528° |
| argument of perigee: | 40.2691° |
| revolutions per day: | 13.04347947 |
| mean anomaly at epoch: | 324.9033° |
| orbit number at epoch: | 6355 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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