View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60286U 26145.17376384 +.00000000 +00000-0 +74399-3 0 00007
2 60286 53.1609 56.9501 0001730 87.2269 272.8930 15.30096146 05
| Epoch (UTC): | 25 May 2026 04:10:13 |
| Eccentricity: | 0.0001730 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 56.9501° |
| argument of perigee: | 87.2269° |
| revolutions per day: | 15.30096146 |
| mean anomaly at epoch: | 272.8930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|