View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43597U 98067PJ 20248.19053934 .05224124 12197-4 75260-3 0 9995
2 43597 51.6102 220.8087 0003266 222.6275 137.4495 16.33928828117760
| Epoch (UTC): | 04 September 2020 04:34:22 |
| Eccentricity: | 0.0003266 |
| inclination: | 51.6102° |
| perigee height: | 180 km |
| apogee height: | 184 km |
| right ascension of ascending node: | 220.8087° |
| argument of perigee: | 222.6275° |
| revolutions per day: | 16.33928828 |
| mean anomaly at epoch: | 137.4495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|