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 16117U 85092C 23269.78199569 .00000043 00000-0 00000-0 0 9993
2 16117 14.7932 353.5863 0008610 124.7653 225.5392 0.98986343 15879
| Epoch (UTC): | 26 September 2023 18:46:04 |
| Eccentricity: | 0.0008610 |
| inclination: | 14.7932° |
| perigee height: | 36114 km |
| apogee height: | 36187 km |
| right ascension of ascending node: | 353.5863° |
| argument of perigee: | 124.7653° |
| revolutions per day: | 0.98986343 |
| mean anomaly at epoch: | 225.5392° |
| orbit number at epoch: | 1587 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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