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 03598U 68110B 22224.79879801 .00000292 00000-0 71150-4 0 9993
2 03598 34.9925 143.7866 0048670 21.9445 338.3320 14.54729699819819
| Epoch (UTC): | 12 August 2022 19:10:16 |
| Eccentricity: | 0.0048670 |
| inclination: | 34.9925° |
| perigee height: | 676 km |
| apogee height: | 745 km |
| right ascension of ascending node: | 143.7866° |
| argument of perigee: | 21.9445° |
| revolutions per day: | 14.54729699 |
| mean anomaly at epoch: | 338.3320° |
| orbit number at epoch: | 81981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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