View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27386U 02009A 23271.93331722 .00000268 00000-0 10159-3 0 9997
2 27386 98.2438 237.7364 0001214 87.9138 337.9743 14.38413520130874
| Epoch (UTC): | 28 September 2023 22:23:58 |
| Eccentricity: | 0.0001214 |
| inclination: | 98.2438° |
| perigee height: | 763 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 237.7364° |
| argument of perigee: | 87.9138° |
| revolutions per day: | 14.38413520 |
| mean anomaly at epoch: | 337.9743° |
| orbit number at epoch: | 13087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|