View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56730U 26145.45696269 +.00000000 +00000-0 +11808-3 0 00000
2 56730 86.6795 43.7695 0002359 81.9681 278.1808 14.80239680 05
| Epoch (UTC): | 25 May 2026 10:58:01 |
| Eccentricity: | 0.0002359 |
| inclination: | 86.6795° |
| perigee height: | 627 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 43.7695° |
| argument of perigee: | 81.9681° |
| revolutions per day: | 14.80239680 |
| mean anomaly at epoch: | 278.1808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|