View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60046U 26145.54462972 +.00000000 +00000-0 -26282-6 0 00003
2 60046 53.1600 247.2726 0001574 116.4737 243.6442 15.69695079 01
| Epoch (UTC): | 25 May 2026 13:04:16 |
| Eccentricity: | 0.0001574 |
| inclination: | 53.1600° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 247.2726° |
| argument of perigee: | 116.4737° |
| revolutions per day: | 15.69695079 |
| mean anomaly at epoch: | 243.6442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|