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 00047U 60007C 23027.63222649 .00000649 00000-0 16619-3 0 9997
2 00047 66.6656 123.0818 0231036 323.6034 34.9545 14.42576063272275
| Epoch (UTC): | 27 January 2023 15:10:24 |
| Eccentricity: | 0.0231036 |
| inclination: | 66.6656° |
| perigee height: | 585 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 123.0818° |
| argument of perigee: | 323.6034° |
| revolutions per day: | 14.42576063 |
| mean anomaly at epoch: | 34.9545° |
| orbit number at epoch: | 27227 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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