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 35815U 09047A 22293.64756977 0.00000000 00000-0 00000-0 0 04
2 35815 0.0370 311.9592 0018650 348.3604 11.6396 1.00241596 06
| Epoch (UTC): | 20 October 2022 15:32:30 |
| Eccentricity: | 0.0018650 |
| inclination: | 0.0370° |
| perigee height: | 35716 km |
| apogee height: | 35873 km |
| right ascension of ascending node: | 311.9592° |
| argument of perigee: | 348.3604° |
| revolutions per day: | 1.00241596 |
| mean anomaly at epoch: | 11.6396° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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