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 36395U 10005A 22225.20168765 -.00000096 00000-0 00000-0 0 9996
2 36395 31.7608 108.3054 0001302 242.7037 301.0389 1.00276070 45988
| Epoch (UTC): | 13 August 2022 04:50:25 |
| Eccentricity: | 0.0001302 |
| inclination: | 31.7608° |
| perigee height: | 35779 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 108.3054° |
| argument of perigee: | 242.7037° |
| revolutions per day: | 1.00276070 |
| mean anomaly at epoch: | 301.0389° |
| orbit number at epoch: | 4598 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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