View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40301U 14070D 23337.65865496 .14329432 24353-5 12164-3 0 9994
2 40301 97.1123 51.9812 0010388 267.5322 92.4795 16.51838351506486
| Epoch (UTC): | 03 December 2023 15:48:27 |
| Eccentricity: | 0.0010388 |
| inclination: | 97.1123° |
| perigee height: | 128 km |
| apogee height: | 141 km |
| right ascension of ascending node: | 51.9812° |
| argument of perigee: | 267.5322° |
| revolutions per day: | 16.51838351 |
| mean anomaly at epoch: | 92.4795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|