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 22027.30026002 .00000728 00000-0 38338-3 0 9998
2 00011 32.8746 4.3031 1466216 336.1731 17.7164 11.85876704344896
| Epoch (UTC): | 27 January 2022 07:12:22 |
| Eccentricity: | 0.1466216 |
| inclination: | 32.8746° |
| perigee height: | 554 km |
| apogee height: | 2935 km |
| right ascension of ascending node: | 4.3031° |
| argument of perigee: | 336.1731° |
| revolutions per day: | 11.85876704 |
| mean anomaly at epoch: | 17.7164° |
| orbit number at epoch: | 34489 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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