View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68905U 26145.50900260 +.00000000 +00000-0 +92858-3 0 00006
2 68905 97.2854 341.2421 0001178 116.1048 244.0325 15.49216658 07
| Epoch (UTC): | 25 May 2026 12:12:57 |
| Eccentricity: | 0.0001178 |
| inclination: | 97.2854° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 341.2421° |
| argument of perigee: | 116.1048° |
| revolutions per day: | 15.49216658 |
| mean anomaly at epoch: | 244.0325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|