View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31114U 26158.76072383 +.00000000 +00000-0 +69513-4 0 00009
2 31114 98.4091 267.5732 0059573 33.3979 327.0934 14.20274125 04
| Epoch (UTC): | 07 June 2026 18:15:26 |
| Eccentricity: | 0.0059573 |
| inclination: | 98.4091° |
| perigee height: | 782 km |
| apogee height: | 867 km |
| right ascension of ascending node: | 267.5732° |
| argument of perigee: | 33.3979° |
| revolutions per day: | 14.20274125 |
| mean anomaly at epoch: | 327.0934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|