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 27597U 02056A 22228.11834537 .00000140 00000-0 74745-4 0 9997
2 27597 98.6086 171.1041 0001131 130.8714 229.2565 14.27633791 24464
| Epoch (UTC): | 16 August 2022 02:50:25 |
| Eccentricity: | 0.0001131 |
| inclination: | 98.6086° |
| perigee height: | 799 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 171.1041° |
| argument of perigee: | 130.8714° |
| revolutions per day: | 14.27633791 |
| mean anomaly at epoch: | 229.2565° |
| orbit number at epoch: | 2446 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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