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 22176.34551292 .00000281 00000-0 15264-3 0 9998
2 00011 32.8639 164.3595 1466518 98.0909 278.8080 11.86142467362592
| Epoch (UTC): | 25 June 2022 08:17:32 |
| Eccentricity: | 0.1466518 |
| inclination: | 32.8639° |
| perigee height: | 552 km |
| apogee height: | 2934 km |
| right ascension of ascending node: | 164.3595° |
| argument of perigee: | 98.0909° |
| revolutions per day: | 11.86142467 |
| mean anomaly at epoch: | 278.8080° |
| orbit number at epoch: | 36259 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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