View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 26065U 26106.79857020 +.00000000 +00000-0 +42127-4 0 00005
2 26065 100.1925 35.9892 0035574 206.0252 153.9142 14.38212257 06
| Epoch (UTC): | 16 April 2026 19:09:56 |
| Eccentricity: | 0.0035574 |
| inclination: | 100.1925° |
| perigee height: | 739 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 35.9892° |
| argument of perigee: | 206.0252° |
| revolutions per day: | 14.38212257 |
| mean anomaly at epoch: | 153.9142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|