View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60935U 26144.93614352 +.00000000 +00000-0 +29950-5 0 00006
2 60935 53.1591 325.6817 0000781 95.2162 264.8945 15.69714239 07
| Epoch (UTC): | 24 May 2026 22:28:02 |
| Eccentricity: | 0.0000781 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 325.6817° |
| argument of perigee: | 95.2162° |
| revolutions per day: | 15.69714239 |
| mean anomaly at epoch: | 264.8945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|