View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25759U 26042.07623896 +.00000000 +00000-0 +80616-4 0 00001
2 25759 98.6301 73.5457 0025521 276.2121 83.6168 14.55757095 04
| Epoch (UTC): | 11 February 2026 01:49:47 |
| Eccentricity: | 0.0025521 |
| inclination: | 98.6301° |
| perigee height: | 689 km |
| apogee height: | 725 km |
| right ascension of ascending node: | 73.5457° |
| argument of perigee: | 276.2121° |
| revolutions per day: | 14.55757095 |
| mean anomaly at epoch: | 83.6168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|