View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19650U 26100.40803602 +.00000000 +00000-0 +13031-3 0 00007
2 19650 70.9979 84.7551 0015766 315.6981 44.2880 14.16159193 08
| Epoch (UTC): | 10 April 2026 09:47:34 |
| Eccentricity: | 0.0015766 |
| inclination: | 70.9979° |
| perigee height: | 827 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 84.7551° |
| argument of perigee: | 315.6981° |
| revolutions per day: | 14.16159193 |
| mean anomaly at epoch: | 44.2880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|