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 16682U 86030B 24287.46335155 .00001082 00000-0 37491-3 0 9993
2 16682 74.0273 351.6857 0013942 36.7146 63.6829 14.36809866 14874
| Epoch (UTC): | 13 October 2024 11:07:13 |
| Eccentricity: | 0.0013942 |
| inclination: | 74.0273° |
| perigee height: | 759 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 351.6857° |
| argument of perigee: | 36.7146° |
| revolutions per day: | 14.36809866 |
| mean anomaly at epoch: | 63.6829° |
| orbit number at epoch: | 1487 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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