View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23659U 26017.32172645 +.00000000 +00000-0 +42702-4 0 00003
2 23659 82.5294 273.2628 0026061 50.2366 43.5066 14.80262182 02
| Epoch (UTC): | 17 January 2026 07:43:17 |
| Eccentricity: | 0.0026061 |
| inclination: | 82.5294° |
| perigee height: | 610 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 273.2628° |
| argument of perigee: | 50.2366° |
| revolutions per day: | 14.80262182 |
| mean anomaly at epoch: | 43.5066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|