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 16986U 86074A 23335.53674314 .00008335 00000-0 45707-3 0 9999
2 16986 82.5334 343.2864 0006509 227.3051 132.7633 15.14025244 5094
| Epoch (UTC): | 01 December 2023 12:52:54 |
| Eccentricity: | 0.0006509 |
| inclination: | 82.5334° |
| perigee height: | 519 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 343.2864° |
| argument of perigee: | 227.3051° |
| revolutions per day: | 15.14025244 |
| mean anomaly at epoch: | 132.7633° |
| orbit number at epoch: | 509 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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