View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20624U 90046A 23154.58124609 -.00000184 00000-0 -71404-4 0 9998
2 20624 71.0409 336.4285 0016939 301.5112 58.4355 14.14468512704770
| Epoch (UTC): | 03 June 2023 13:56:59 |
| Eccentricity: | 0.0016939 |
| inclination: | 71.0409° |
| perigee height: | 832 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 336.4285° |
| argument of perigee: | 301.5112° |
| revolutions per day: | 14.14468512 |
| mean anomaly at epoch: | 58.4355° |
| orbit number at epoch: | 70477 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|