View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45436U 26145.38665438 +.00000000 +00000-0 -14734-2 0 00008
2 45436 87.8917 25.6033 0002039 104.6799 255.4555 13.11417992 02
| Epoch (UTC): | 25 May 2026 09:16:46 |
| Eccentricity: | 0.0002039 |
| inclination: | 87.8917° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6033° |
| argument of perigee: | 104.6799° |
| revolutions per day: | 13.11417992 |
| mean anomaly at epoch: | 255.4555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|