View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 09661U 26121.92690970 +.00000000 +00000-0 +11557-3 0 00001
2 09661 81.2624 138.4971 0011379 118.9068 241.3243 14.04219416 05
| Epoch (UTC): | 01 May 2026 22:14:44 |
| Eccentricity: | 0.0011379 |
| inclination: | 81.2624° |
| perigee height: | 871 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 138.4971° |
| argument of perigee: | 118.9068° |
| revolutions per day: | 14.04219416 |
| mean anomaly at epoch: | 241.3243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|