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 05560U 71089A 22137.72794358 .00000472 00000-0 12649-3 0 9999
2 05560 92.7255 62.2719 0018551 95.5477 264.7844 14.48273493660688
| Epoch (UTC): | 17 May 2022 17:28:14 |
| Eccentricity: | 0.0018551 |
| inclination: | 92.7255° |
| perigee height: | 718 km |
| apogee height: | 744 km |
| right ascension of ascending node: | 62.2719° |
| argument of perigee: | 95.5477° |
| revolutions per day: | 14.48273493 |
| mean anomaly at epoch: | 264.7844° |
| orbit number at epoch: | 66068 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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