View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 41917U 17003A 23150.86900125 .00000258 00000-0 85166-4 0 9990
2 41917 86.4010 193.7554 0002322 83.2613 276.8847 14.34221784333635
| Epoch (UTC): | 30 May 2023 20:51:21 |
| Eccentricity: | 0.0002322 |
| inclination: | 86.4010° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 193.7554° |
| argument of perigee: | 83.2613° |
| revolutions per day: | 14.34221784 |
| mean anomaly at epoch: | 276.8847° |
| orbit number at epoch: | 33363 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|