View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41786U 26150.59146631 +.00000000 +00000-0 +14694-3 0 00005
2 41786 97.9909 213.2011 0000777 88.1319 271.9977 14.70846266 08
| Epoch (UTC): | 30 May 2026 14:11:42 |
| Eccentricity: | 0.0000777 |
| inclination: | 97.9909° |
| perigee height: | 658 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 213.2011° |
| argument of perigee: | 88.1319° |
| revolutions per day: | 14.70846266 |
| mean anomaly at epoch: | 271.9977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|