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 36340U 82025AA 22224.19279777 .00002477 00000-0 10637-2 0 9993
2 36340 82.5280 205.9910 0025922 1.5439 358.5818 14.24257037461780
| Epoch (UTC): | 12 August 2022 04:37:37 |
| Eccentricity: | 0.0025922 |
| inclination: | 82.5280° |
| perigee height: | 792 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 205.9910° |
| argument of perigee: | 1.5439° |
| revolutions per day: | 14.24257037 |
| mean anomaly at epoch: | 358.5818° |
| orbit number at epoch: | 46178 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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