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 23026.59227819 .00000743 00000-0 18662-3 0 9990
2 00047 66.6656 125.8648 0230966 324.3484 34.2376 14.42574770272126
| Epoch (UTC): | 26 January 2023 14:12:52 |
| Eccentricity: | 0.0230966 |
| inclination: | 66.6656° |
| perigee height: | 585 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 125.8648° |
| argument of perigee: | 324.3484° |
| revolutions per day: | 14.42574770 |
| mean anomaly at epoch: | 34.2376° |
| orbit number at epoch: | 27212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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