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 47311U 21002C 22176.59662326 .00005350 00000-0 22012-3 0 9991
2 47311 60.6858 331.5899 0017661 342.6660 17.3823 15.25416061 79705
| Epoch (UTC): | 25 June 2022 14:19:08 |
| Eccentricity: | 0.0017661 |
| inclination: | 60.6858° |
| perigee height: | 477 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 331.5899° |
| argument of perigee: | 342.6660° |
| revolutions per day: | 15.25416061 |
| mean anomaly at epoch: | 17.3823° |
| orbit number at epoch: | 7970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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