View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59403U 26145.24447242 +.00000000 +00000-0 +18250-3 0 00000
2 59403 43.0033 343.8512 0000971 265.7771 94.2970 15.27579826 07
| Epoch (UTC): | 25 May 2026 05:52:02 |
| Eccentricity: | 0.0000971 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 343.8512° |
| argument of perigee: | 265.7771° |
| revolutions per day: | 15.27579826 |
| mean anomaly at epoch: | 94.2970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|