View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68709U 26145.40816843 +.00000000 +00000-0 +10520-2 0 00005
2 68709 53.1597 38.1116 0000923 90.5744 269.5370 15.49332938 04
| Epoch (UTC): | 25 May 2026 09:47:45 |
| Eccentricity: | 0.0000923 |
| inclination: | 53.1597° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 38.1116° |
| argument of perigee: | 90.5744° |
| revolutions per day: | 15.49332938 |
| mean anomaly at epoch: | 269.5370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|