View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53605U 26145.50003470 +.00000000 +00000-0 +34517-2 0 00001
2 53605 53.2168 241.5215 0001130 47.7629 269.6429 15.74440235 09
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.2168° |
| perigee height: | 345 km |
| apogee height: | 347 km |
| right ascension of ascending node: | 241.5215° |
| argument of perigee: | 47.7629° |
| revolutions per day: | 15.74440235 |
| mean anomaly at epoch: | 269.6429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|