View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42786U 17036X 24107.15615470 .18333050 24204-5 21342-3 0 9992
2 42786 97.0810 147.7264 0011072 260.2035 99.8020 16.49662273380223
| Epoch (UTC): | 16 April 2024 03:44:51 |
| Eccentricity: | 0.0011072 |
| inclination: | 97.0810° |
| perigee height: | 133 km |
| apogee height: | 147 km |
| right ascension of ascending node: | 147.7264° |
| argument of perigee: | 260.2035° |
| revolutions per day: | 16.49662273 |
| mean anomaly at epoch: | 99.8020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|