View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60513U 26145.49746811 +.00000000 +00000-0 +28143-3 0 00007
2 60513 97.3824 227.3450 0004435 45.6280 314.5326 15.33990116 06
| Epoch (UTC): | 25 May 2026 11:56:21 |
| Eccentricity: | 0.0004435 |
| inclination: | 97.3824° |
| perigee height: | 461 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 227.3450° |
| argument of perigee: | 45.6280° |
| revolutions per day: | 15.33990116 |
| mean anomaly at epoch: | 314.5326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|