View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 226U 62002A 23334.20604416 .00000776 00000-0 25405-3 0 9997
2 226 48.2961 257.7910 0077335 21.4830 338.9286 14.46194483254673
| Epoch (UTC): | 30 November 2023 04:56:42 |
| Eccentricity: | 0.0077335 |
| inclination: | 48.2961° |
| perigee height: | 683 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 257.7910° |
| argument of perigee: | 21.4830° |
| revolutions per day: | 14.46194483 |
| mean anomaly at epoch: | 338.9286° |
| orbit number at epoch: | 25467 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|