View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60106U 26145.42442738 +.00000000 +00000-0 +42024-6 0 00006
2 60106 53.1618 40.7876 0001221 100.1924 259.9214 15.30189875 03
| Epoch (UTC): | 25 May 2026 10:11:10 |
| Eccentricity: | 0.0001221 |
| inclination: | 53.1618° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.7876° |
| argument of perigee: | 100.1924° |
| revolutions per day: | 15.30189875 |
| mean anomaly at epoch: | 259.9214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|