View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 40376U 15003A 23152.90000659 .00000619 00000-0 12892-3 0 9992
2 40376 98.1272 159.6866 0001296 89.4927 270.6423 14.63381684445099
| Epoch (UTC): | 01 June 2023 21:36:00 |
| Eccentricity: | 0.0001296 |
| inclination: | 98.1272° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 159.6866° |
| argument of perigee: | 89.4927° |
| revolutions per day: | 14.63381684 |
| mean anomaly at epoch: | 270.6423° |
| orbit number at epoch: | 44509 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|