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 23340.50569322 .00058370 00000-0 86692-3 0 9992
2 47311 60.6744 109.8787 0024331 39.3572 320.9292 15.54452414160916
| Epoch (UTC): | 06 December 2023 12:08:11 |
| Eccentricity: | 0.0024331 |
| inclination: | 60.6744° |
| perigee height: | 387 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 109.8787° |
| argument of perigee: | 39.3572° |
| revolutions per day: | 15.54452414 |
| mean anomaly at epoch: | 320.9292° |
| orbit number at epoch: | 16091 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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