View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41917U 26038.81442351 +.00000000 +00000-0 -55179-5 0 00005
2 41917 86.4023 142.6336 0001718 90.1139 270.0253 14.34217672 08
| Epoch (UTC): | 07 February 2026 19:32:46 |
| Eccentricity: | 0.0001718 |
| inclination: | 86.4023° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 142.6336° |
| argument of perigee: | 90.1139° |
| revolutions per day: | 14.34217672 |
| mean anomaly at epoch: | 270.0253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|