View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53436U 26145.23251083 +.00000000 +00000-0 -82096-5 0 00007
2 53436 53.2145 120.1884 0001133 84.2521 275.8601 15.08839624 02
| Epoch (UTC): | 25 May 2026 05:34:48 |
| Eccentricity: | 0.0001133 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 120.1884° |
| argument of perigee: | 84.2521° |
| revolutions per day: | 15.08839624 |
| mean anomaly at epoch: | 275.8601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|