View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22826U 26053.12723984 +.00000000 +00000-0 +51701-4 0 00003
2 22826 98.6965 120.4289 0009885 65.3500 294.8711 14.31330786 08
| Epoch (UTC): | 22 February 2026 03:03:13 |
| Eccentricity: | 0.0009885 |
| inclination: | 98.6965° |
| perigee height: | 780 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 120.4289° |
| argument of perigee: | 65.3500° |
| revolutions per day: | 14.31330786 |
| mean anomaly at epoch: | 294.8711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|