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 22144.56344539 .00000518 00000-0 12248-3 0 9997
2 03598 34.9927 237.1512 0048529 91.1401 269.4852 14.54683700808129
| Epoch (UTC): | 24 May 2022 13:31:21 |
| Eccentricity: | 0.0048529 |
| inclination: | 34.9927° |
| perigee height: | 676 km |
| apogee height: | 745 km |
| right ascension of ascending node: | 237.1512° |
| argument of perigee: | 91.1401° |
| revolutions per day: | 14.54683700 |
| mean anomaly at epoch: | 269.4852° |
| orbit number at epoch: | 80812 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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