View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20U 59007A 23089.08831744 .00004668 00000-0 18805-2 0 9998
2 20 33.3531 161.8522 1659847 257.4034 83.6641 11.57186233348192
| Epoch (UTC): | 30 March 2023 02:07:10 |
| Eccentricity: | 0.1659847 |
| inclination: | 33.3531° |
| perigee height: | 508 km |
| apogee height: | 3249 km |
| right ascension of ascending node: | 161.8522° |
| argument of perigee: | 257.4034° |
| revolutions per day: | 11.57186233 |
| mean anomaly at epoch: | 83.6641° |
| orbit number at epoch: | 34819 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|