View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52358U 26145.56788891 +.00000000 +00000-0 -29519-4 0 00007
2 52358 53.2111 214.0021 0001176 85.0514 275.0613 15.08835480 02
| Epoch (UTC): | 25 May 2026 13:37:45 |
| Eccentricity: | 0.0001176 |
| inclination: | 53.2111° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 214.0021° |
| argument of perigee: | 85.0514° |
| revolutions per day: | 15.08835480 |
| mean anomaly at epoch: | 275.0613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|