View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00116U 26134.49525875 +.00000000 +00000-0 +44002-4 0 00006
2 00116 66.8101 333.2748 0081586 294.5921 64.6673 13.92325930 01
| Epoch (UTC): | 14 May 2026 11:53:10 |
| Eccentricity: | 0.0081586 |
| inclination: | 66.8101° |
| perigee height: | 861 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 333.2748° |
| argument of perigee: | 294.5921° |
| revolutions per day: | 13.92325930 |
| mean anomaly at epoch: | 64.6673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|