View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58442U 26145.23085877 +.00000000 +00000-0 +52577-4 0 00004
2 58442 43.0045 329.0735 0000532 305.3003 54.7798 15.27573221 09
| Epoch (UTC): | 25 May 2026 05:32:26 |
| Eccentricity: | 0.0000532 |
| inclination: | 43.0045° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 329.0735° |
| argument of perigee: | 305.3003° |
| revolutions per day: | 15.27573221 |
| mean anomaly at epoch: | 54.7798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|