View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58672U 26145.32942823 +.00000000 +00000-0 +23975-2 0 00000
2 58672 42.9945 3.0613 0021544 262.0527 97.7887 15.47889232 01
| Epoch (UTC): | 25 May 2026 07:54:22 |
| Eccentricity: | 0.0021544 |
| inclination: | 42.9945° |
| perigee height: | 408 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 3.0613° |
| argument of perigee: | 262.0527° |
| revolutions per day: | 15.47889232 |
| mean anomaly at epoch: | 97.7887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|