View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25544U 26109.16735170 +.00000000 +00000-0 +15944-3 0 00007
2 25544 51.6330 232.2024 0006622 324.6287 35.4262 15.48825421 05
| Epoch (UTC): | 19 April 2026 04:00:59 |
| Eccentricity: | 0.0006622 |
| inclination: | 51.6330° |
| perigee height: | 416 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 232.2024° |
| argument of perigee: | 324.6287° |
| revolutions per day: | 15.48825421 |
| mean anomaly at epoch: | 35.4262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|