View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 11289U 26100.16798727 +.00000000 +00000-0 +74649-5 0 00005
2 11289 81.2438 262.9047 0075949 97.1406 263.8409 14.12105604 06
| Epoch (UTC): | 10 April 2026 04:01:54 |
| Eccentricity: | 0.0075949 |
| inclination: | 81.2438° |
| perigee height: | 797 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 262.9047° |
| argument of perigee: | 97.1406° |
| revolutions per day: | 14.12105604 |
| mean anomaly at epoch: | 263.8409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|