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 22016.97766144 .00000106 00000-0 48584-4 0 9992
2 27386 98.1677 5.3274 0001198 86.1905 291.4443 14.38068987 41764
| Epoch (UTC): | 16 January 2022 23:27:49 |
| Eccentricity: | 0.0001198 |
| inclination: | 98.1677° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 5.3274° |
| argument of perigee: | 86.1905° |
| revolutions per day: | 14.38068987 |
| mean anomaly at epoch: | 291.4443° |
| orbit number at epoch: | 4176 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|