View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20433U 26088.15153774 +.00000000 +00000-0 +10769-3 0 00008
2 20433 74.0357 224.8897 0041013 291.3073 240.9636 14.37514220 03
| Epoch (UTC): | 29 March 2026 03:38:12 |
| Eccentricity: | 0.0041013 |
| inclination: | 74.0357° |
| perigee height: | 737 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 224.8897° |
| argument of perigee: | 291.3073° |
| revolutions per day: | 14.37514220 |
| mean anomaly at epoch: | 240.9636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|