View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 03271U 26100.02986522 +.00000000 +00000-0 +81763-4 0 00008
2 03271 98.5684 276.7125 0051963 27.8353 332.5586 14.17611233 08
| Epoch (UTC): | 10 April 2026 00:43:00 |
| Eccentricity: | 0.0051963 |
| inclination: | 98.5684° |
| perigee height: | 796 km |
| apogee height: | 871 km |
| right ascension of ascending node: | 276.7125° |
| argument of perigee: | 27.8353° |
| revolutions per day: | 14.17611233 |
| mean anomaly at epoch: | 332.5586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|