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 11U 59001A 22147.03784739 .00000482 00000-0 23907-3 0 9992
2 11 32.8778 274.4913 1467180 292.4902 52.7038 11.86124137700853
| Epoch (UTC): | 27 May 2022 00:54:30 |
| Eccentricity: | 0.1467180 |
| inclination: | 32.8778° |
| perigee height: | 552 km |
| apogee height: | 2935 km |
| right ascension of ascending node: | 274.4913° |
| argument of perigee: | 292.4902° |
| revolutions per day: | 11.86124137 |
| mean anomaly at epoch: | 52.7038° |
| orbit number at epoch: | 70085 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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