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 22022.07744169 .00000743 00000-0 38448-3 0 9997
2 00011 32.8783 23.9148 1466442 306.6810 40.7578 11.85869111344275
| Epoch (UTC): | 22 January 2022 01:51:30 |
| Eccentricity: | 0.1466442 |
| inclination: | 32.8783° |
| perigee height: | 553 km |
| apogee height: | 2936 km |
| right ascension of ascending node: | 23.9148° |
| argument of perigee: | 306.6810° |
| revolutions per day: | 11.85869111 |
| mean anomaly at epoch: | 40.7578° |
| orbit number at epoch: | 34427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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