View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66679U 26145.16658765 +.00000000 +00000-0 +97390-4 0 00001
2 66679 97.4160 218.6733 0007730 89.0117 271.2003 15.17813739 06
| Epoch (UTC): | 25 May 2026 03:59:53 |
| Eccentricity: | 0.0007730 |
| inclination: | 97.4160° |
| perigee height: | 507 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 218.6733° |
| argument of perigee: | 89.0117° |
| revolutions per day: | 15.17813739 |
| mean anomaly at epoch: | 271.2003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|