View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41918U 26156.57099677 +.00000000 +00000-0 +33254-4 0 00007
2 41918 86.3960 93.3116 0002462 82.1785 277.9690 14.34218703 08
| Epoch (UTC): | 05 June 2026 13:42:14 |
| Eccentricity: | 0.0002462 |
| inclination: | 86.3960° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 93.3116° |
| argument of perigee: | 82.1785° |
| revolutions per day: | 14.34218703 |
| mean anomaly at epoch: | 277.9690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|