View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00053U 60009E 22148.47791784 -.00000122 00000-0 -35707-3 0 9999
2 00053 47.2750 229.3483 0096910 19.1413 341.2980 12.17270501755055
| Epoch (UTC): | 28 May 2022 11:28:12 |
| Eccentricity: | 0.0096910 |
| inclination: | 47.2750° |
| perigee height: | 1527 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 229.3483° |
| argument of perigee: | 19.1413° |
| revolutions per day: | 12.17270501 |
| mean anomaly at epoch: | 341.2980° |
| orbit number at epoch: | 75505 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|