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 26722U 01011D 23342.53559795 -.00000113 00000-0 -84728-2 0 9992
2 26722 1.8398 287.0457 7062004 216.4677 7.0273 2.22912675185341
| Epoch (UTC): | 08 December 2023 12:51:15 |
| Eccentricity: | 0.7062004 |
| inclination: | 1.8398° |
| perigee height: | 894 km |
| apogee height: | 35857 km |
| right ascension of ascending node: | 287.0457° |
| argument of perigee: | 216.4677° |
| revolutions per day: | 2.22912675 |
| mean anomaly at epoch: | 7.0273° |
| orbit number at epoch: | 18534 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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