View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68511U 26145.30852097 +.00000000 +00000-0 +10287-2 0 00006
2 68511 53.1578 127.0158 0001276 112.6496 247.4648 15.49334253 05
| Epoch (UTC): | 25 May 2026 07:24:16 |
| Eccentricity: | 0.0001276 |
| inclination: | 53.1578° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 127.0158° |
| argument of perigee: | 112.6496° |
| revolutions per day: | 15.49334253 |
| mean anomaly at epoch: | 247.4648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|