View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68482U 26145.34336282 +.00000000 +00000-0 +29444-3 0 00006
2 68482 97.7555 104.0128 0003041 0.1965 359.9255 14.92758167 01
| Epoch (UTC): | 25 May 2026 08:14:26 |
| Eccentricity: | 0.0003041 |
| inclination: | 97.7555° |
| perigee height: | 587 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 104.0128° |
| argument of perigee: | 0.1965° |
| revolutions per day: | 14.92758167 |
| mean anomaly at epoch: | 359.9255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|