View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 40024U 14033Q 23090.10048171 .00012295 00000-0 11332-2 0 9998
2 40024 98.0207 43.3711 0011025 169.6553 190.4895 14.94795629477269
| Epoch (UTC): | 31 March 2023 02:24:41 |
| Eccentricity: | 0.0011025 |
| inclination: | 98.0207° |
| perigee height: | 575 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 43.3711° |
| argument of perigee: | 169.6553° |
| revolutions per day: | 14.94795629 |
| mean anomaly at epoch: | 190.4895° |
| orbit number at epoch: | 47726 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|