View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60071U 26145.37936948 +.00000000 +00000-0 +79777-5 0 00006
2 60071 53.1596 173.3811 0001178 68.6196 291.4948 15.69704061 08
| Epoch (UTC): | 25 May 2026 09:06:17 |
| Eccentricity: | 0.0001178 |
| inclination: | 53.1596° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 173.3811° |
| argument of perigee: | 68.6196° |
| revolutions per day: | 15.69704061 |
| mean anomaly at epoch: | 291.4948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|