View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68827U 26145.62480058 +.00000000 +00000-0 +17404-3 0 00004
2 68827 96.6465 64.1182 0017940 121.0846 239.2188 15.81548512 07
| Epoch (UTC): | 25 May 2026 14:59:42 |
| Eccentricity: | 0.0017940 |
| inclination: | 96.6465° |
| perigee height: | 314 km |
| apogee height: | 338 km |
| right ascension of ascending node: | 64.1182° |
| argument of perigee: | 121.0846° |
| revolutions per day: | 15.81548512 |
| mean anomaly at epoch: | 239.2188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|