View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41917U 26039.37257176 +.00000000 +00000-0 -82671-5 0 00003
2 41917 86.4023 142.4008 0001736 90.6629 269.4766 14.34217596 07
| Epoch (UTC): | 08 February 2026 08:56:30 |
| Eccentricity: | 0.0001736 |
| inclination: | 86.4023° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 142.4008° |
| argument of perigee: | 90.6629° |
| revolutions per day: | 14.34217596 |
| mean anomaly at epoch: | 269.4766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|