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 39086U 13009A 23275.12564827 .00000219 00000-0 97232-4 0 9992
2 39086 98.5495 98.8796 0001698 5.5737 354.5465 14.32267519553999
| Epoch (UTC): | 02 October 2023 03:00:56 |
| Eccentricity: | 0.0001698 |
| inclination: | 98.5495° |
| perigee height: | 783 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 98.8796° |
| argument of perigee: | 5.5737° |
| revolutions per day: | 14.32267519 |
| mean anomaly at epoch: | 354.5465° |
| orbit number at epoch: | 55399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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