View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31114U 26138.18963299 +.00000000 +00000-0 +47449-4 0 00002
2 31114 98.4067 248.0129 0060196 92.2326 268.5746 14.20268302 04
| Epoch (UTC): | 18 May 2026 04:33:04 |
| Eccentricity: | 0.0060196 |
| inclination: | 98.4067° |
| perigee height: | 781 km |
| apogee height: | 868 km |
| right ascension of ascending node: | 248.0129° |
| argument of perigee: | 92.2326° |
| revolutions per day: | 14.20268302 |
| mean anomaly at epoch: | 268.5746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|