View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61619U 26145.63660435 +.00000000 +00000-0 +11547-3 0 00008
2 61619 34.9964 339.8957 0005289 151.4877 208.6128 15.23041075 06
| Epoch (UTC): | 25 May 2026 15:16:42 |
| Eccentricity: | 0.0005289 |
| inclination: | 34.9964° |
| perigee height: | 493 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 339.8957° |
| argument of perigee: | 151.4877° |
| revolutions per day: | 15.23041075 |
| mean anomaly at epoch: | 208.6128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|