View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 40042U 14033AJ 23033.42264546 .00005675 00000-0 55904-3 0 9994
2 40042 97.9944 339.6308 0014293 19.5100 340.6662 14.92381468467922
| Epoch (UTC): | 02 February 2023 10:08:36 |
| Eccentricity: | 0.0014293 |
| inclination: | 97.9944° |
| perigee height: | 580 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 339.6308° |
| argument of perigee: | 19.5100° |
| revolutions per day: | 14.92381468 |
| mean anomaly at epoch: | 340.6662° |
| orbit number at epoch: | 46792 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|