View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68077U 26145.46438051 +.00000000 +00000-0 +44822-3 0 00003
2 68077 53.1577 179.6931 0001140 92.6931 267.4202 15.34397300 08
| Epoch (UTC): | 25 May 2026 11:08:42 |
| Eccentricity: | 0.0001140 |
| inclination: | 53.1577° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 179.6931° |
| argument of perigee: | 92.6931° |
| revolutions per day: | 15.34397300 |
| mean anomaly at epoch: | 267.4202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|