View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68945U 26145.58335647 +.00000000 +00000-0 +15282-2 0 00004
2 68945 51.8784 177.0673 0013912 65.9796 147.5853 15.29763955 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0013912 |
| inclination: | 51.8784° |
| perigee height: | 467 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 177.0673° |
| argument of perigee: | 65.9796° |
| revolutions per day: | 15.29763955 |
| mean anomaly at epoch: | 147.5853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|