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 26549U 00057E 22222.50803022 .00000421 00000-0 67634-4 0 9995
2 26549 64.5511 58.5723 0032998 334.7830 25.1664 14.84216112182600
| Epoch (UTC): | 10 August 2022 12:11:33 |
| Eccentricity: | 0.0032998 |
| inclination: | 64.5511° |
| perigee height: | 593 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 58.5723° |
| argument of perigee: | 334.7830° |
| revolutions per day: | 14.84216112 |
| mean anomaly at epoch: | 25.1664° |
| orbit number at epoch: | 18260 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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