View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59243U 26145.49642145 +.00000000 +00000-0 +78227-4 0 00009
2 59243 43.0002 69.6897 0001283 274.3088 85.7617 15.27580253 07
| Epoch (UTC): | 25 May 2026 11:54:50 |
| Eccentricity: | 0.0001283 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.6897° |
| argument of perigee: | 274.3088° |
| revolutions per day: | 15.27580253 |
| mean anomaly at epoch: | 85.7617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|