View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42846U 26145.40816145 +.00000000 +00000-0 +24643-3 0 00006
2 42846 97.4039 307.6497 0013053 184.3402 175.7715 15.06119611 02
| Epoch (UTC): | 25 May 2026 09:47:45 |
| Eccentricity: | 0.0013053 |
| inclination: | 97.4039° |
| perigee height: | 539 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 307.6497° |
| argument of perigee: | 184.3402° |
| revolutions per day: | 15.06119611 |
| mean anomaly at epoch: | 175.7715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|