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 26609U 00072B 22279.24932655 -.00000028 00000-0 00000+0 0 9990
2 26609 5.6186 243.2346 7977518 64.1779 354.8471 1.25588857100689
| Epoch (UTC): | 06 October 2022 05:59:01 |
| Eccentricity: | 0.7977518 |
| inclination: | 5.6186° |
| perigee height: | 961 km |
| apogee height: | 58859 km |
| right ascension of ascending node: | 243.2346° |
| argument of perigee: | 64.1779° |
| revolutions per day: | 1.25588857 |
| mean anomaly at epoch: | 354.8471° |
| orbit number at epoch: | 10068 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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