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 00011U 59001A 22219.53239186 .00000098 00000-0 45900-4 0 9999
2 00011 32.8745 2.0901 1466599 342.0730 13.2969 11.86159513367729
| Epoch (UTC): | 07 August 2022 12:46:38 |
| Eccentricity: | 0.1466599 |
| inclination: | 32.8745° |
| perigee height: | 552 km |
| apogee height: | 2934 km |
| right ascension of ascending node: | 2.0901° |
| argument of perigee: | 342.0730° |
| revolutions per day: | 11.86159513 |
| mean anomaly at epoch: | 13.2969° |
| orbit number at epoch: | 36772 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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