View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 41918U 17003B 23151.83307881 .00000275 00000-0 91137-4 0 9993
2 41918 86.4008 193.2565 0002645 87.6110 272.5389 14.34220225333798
| Epoch (UTC): | 31 May 2023 19:59:38 |
| Eccentricity: | 0.0002645 |
| inclination: | 86.4008° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 193.2565° |
| argument of perigee: | 87.6110° |
| revolutions per day: | 14.34220225 |
| mean anomaly at epoch: | 272.5389° |
| orbit number at epoch: | 33379 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|