View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60530U 26144.96915051 +.00000000 +00000-0 +15679-3 0 00001
2 60530 97.6794 220.0714 0001930 87.9879 272.1563 14.96326445 05
| Epoch (UTC): | 24 May 2026 23:15:34 |
| Eccentricity: | 0.0001930 |
| inclination: | 97.6794° |
| perigee height: | 577 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 220.0714° |
| argument of perigee: | 87.9879° |
| revolutions per day: | 14.96326445 |
| mean anomaly at epoch: | 272.1563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|