View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41622U 26108.55923787 +.00000000 +00000-0 +00000-0 0 00001
2 41622 2.3340 300.5700 0194773 261.8997 100.6672 1.00271313 07
| Epoch (UTC): | 18 April 2026 13:25:18 |
| Eccentricity: | 0.0194773 |
| inclination: | 2.3340° |
| perigee height: | 34965 km |
| apogee height: | 36608 km |
| right ascension of ascending node: | 300.5700° |
| argument of perigee: | 261.8997° |
| revolutions per day: | 1.00271313 |
| mean anomaly at epoch: | 100.6672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|