View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68979U 26145.58335647 +.00000000 +00000-0 -30658-1 0 00005
2 68979 53.1595 268.1505 0000910 77.7762 344.5067 15.55870485 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000910 |
| inclination: | 53.1595° |
| perigee height: | 399 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 268.1505° |
| argument of perigee: | 77.7762° |
| revolutions per day: | 15.55870485 |
| mean anomaly at epoch: | 344.5067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|