View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25991U 26106.89484860 +.00000000 +00000-0 +64859-4 0 00007
2 25991 99.0027 144.6672 0010247 171.1164 291.6133 14.17540150 03
| Epoch (UTC): | 16 April 2026 21:28:34 |
| Eccentricity: | 0.0010247 |
| inclination: | 99.0027° |
| perigee height: | 826 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 144.6672° |
| argument of perigee: | 171.1164° |
| revolutions per day: | 14.17540150 |
| mean anomaly at epoch: | 291.6133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|