View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55431U 26145.36658361 +.00000000 +00000-0 +31003-4 0 00008
2 55431 69.9994 251.2841 0003191 268.6101 91.4693 14.98330818 04
| Epoch (UTC): | 25 May 2026 08:47:52 |
| Eccentricity: | 0.0003191 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 251.2841° |
| argument of perigee: | 268.6101° |
| revolutions per day: | 14.98330818 |
| mean anomaly at epoch: | 91.4693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|