View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68335U 26145.54925919 +.00000000 +00000-0 +79818-3 0 00006
2 68335 53.1589 346.9556 0001268 96.3374 263.7780 15.49347357 06
| Epoch (UTC): | 25 May 2026 13:10:55 |
| Eccentricity: | 0.0001268 |
| inclination: | 53.1589° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 346.9556° |
| argument of perigee: | 96.3374° |
| revolutions per day: | 15.49347357 |
| mean anomaly at epoch: | 263.7780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|