View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59745U 26145.38368814 +.00000000 +00000-0 -14313-4 0 00009
2 59745 43.0008 110.0095 0001042 273.8477 86.2256 15.27577016 08
| Epoch (UTC): | 25 May 2026 09:12:30 |
| Eccentricity: | 0.0001042 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.0095° |
| argument of perigee: | 273.8477° |
| revolutions per day: | 15.27577016 |
| mean anomaly at epoch: | 86.2256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|