View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59253U 26145.48871262 +.00000000 +00000-0 -10303-4 0 00005
2 59253 43.0019 69.6326 0000917 266.9871 93.0876 15.27579772 06
| Epoch (UTC): | 25 May 2026 11:43:44 |
| Eccentricity: | 0.0000917 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.6326° |
| argument of perigee: | 266.9871° |
| revolutions per day: | 15.27579772 |
| mean anomaly at epoch: | 93.0876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|