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 36796U 10035B 22222.46236080 .00001272 00000-0 14135-3 0 9998
2 36796 98.2239 48.8944 0011727 328.1145 31.9359 14.89059325654815
| Epoch (UTC): | 10 August 2022 11:05:47 |
| Eccentricity: | 0.0011727 |
| inclination: | 98.2239° |
| perigee height: | 592 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 48.8944° |
| argument of perigee: | 328.1145° |
| revolutions per day: | 14.89059325 |
| mean anomaly at epoch: | 31.9359° |
| orbit number at epoch: | 65481 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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