View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53594U 26145.66668980 +.00000000 +00000-0 +40228-2 0 00004
2 53594 53.2169 240.7442 0001219 41.9575 115.5378 15.74980223 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001219 |
| inclination: | 53.2169° |
| perigee height: | 344 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 240.7442° |
| argument of perigee: | 41.9575° |
| revolutions per day: | 15.74980223 |
| mean anomaly at epoch: | 115.5378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|