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 36799U 10035E 22272.59552010 .00003190 00000-0 30995-3 0 9997
2 36799 98.1697 127.1159 0012840 111.0148 249.2445 14.93308753663304
| Epoch (UTC): | 29 September 2022 14:17:32 |
| Eccentricity: | 0.0012840 |
| inclination: | 98.1697° |
| perigee height: | 578 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 127.1159° |
| argument of perigee: | 111.0148° |
| revolutions per day: | 14.93308753 |
| mean anomaly at epoch: | 249.2445° |
| orbit number at epoch: | 66330 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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