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 36108U 09068A 23268.01230152 -.00000277 00000-0 00000+0 0 9992
2 36108 0.1916 91.0334 0000226 332.7035 261.4965 1.00270160 50511
| Epoch (UTC): | 25 September 2023 00:17:42 |
| Eccentricity: | 0.0000226 |
| inclination: | 0.1916° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 91.0334° |
| argument of perigee: | 332.7035° |
| revolutions per day: | 1.00270160 |
| mean anomaly at epoch: | 261.4965° |
| orbit number at epoch: | 5051 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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