View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61189U 26145.56787940 +.00000000 +00000-0 +21037-3 0 00008
2 61189 97.5566 235.4349 0004385 114.0245 246.1443 15.08698446 07
| Epoch (UTC): | 25 May 2026 13:37:44 |
| Eccentricity: | 0.0004385 |
| inclination: | 97.5566° |
| perigee height: | 537 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 235.4349° |
| argument of perigee: | 114.0245° |
| revolutions per day: | 15.08698446 |
| mean anomaly at epoch: | 246.1443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|