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 21022.61254341 .00000052 00000-0 16786-4 0 9993
2 03598 34.9937 108.0044 0048654 99.5993 261.0201 14.54505449737189
| Epoch (UTC): | 22 January 2021 14:42:03 |
| Eccentricity: | 0.0048654 |
| inclination: | 34.9937° |
| perigee height: | 676 km |
| apogee height: | 745 km |
| right ascension of ascending node: | 108.0044° |
| argument of perigee: | 99.5993° |
| revolutions per day: | 14.54505449 |
| mean anomaly at epoch: | 261.0201° |
| orbit number at epoch: | 73718 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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