View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43925U 26145.09332138 +.00000000 +00000-0 +81981-5 0 00005
2 43925 86.3982 3.2191 0002281 86.3053 273.8403 14.34217821 05
| Epoch (UTC): | 25 May 2026 02:14:22 |
| Eccentricity: | 0.0002281 |
| inclination: | 86.3982° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 3.2191° |
| argument of perigee: | 86.3053° |
| revolutions per day: | 14.34217821 |
| mean anomaly at epoch: | 273.8403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|