View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41922U 26129.48812641 +.00000000 +00000-0 +19047-4 0 00000
2 41922 86.3934 104.6608 0002323 94.0315 266.1147 14.34216952 04
| Epoch (UTC): | 09 May 2026 11:42:54 |
| Eccentricity: | 0.0002323 |
| inclination: | 86.3934° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 104.6608° |
| argument of perigee: | 94.0315° |
| revolutions per day: | 14.34216952 |
| mean anomaly at epoch: | 266.1147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|