View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59410U 26145.24063325 +.00000000 +00000-0 -11391-4 0 00005
2 59410 43.0039 343.8199 0000828 270.5835 89.4922 15.27568837 01
| Epoch (UTC): | 25 May 2026 05:46:30 |
| Eccentricity: | 0.0000828 |
| inclination: | 43.0039° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 343.8199° |
| argument of perigee: | 270.5835° |
| revolutions per day: | 15.27568837 |
| mean anomaly at epoch: | 89.4922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|