View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25397U 26154.57772250 +.00000000 +00000-0 +49972-4 0 00007
2 25397 99.0064 146.9934 0000319 213.6137 146.5021 14.24425649 08
| Epoch (UTC): | 03 June 2026 13:51:55 |
| Eccentricity: | 0.0000319 |
| inclination: | 99.0064° |
| perigee height: | 810 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 146.9934° |
| argument of perigee: | 213.6137° |
| revolutions per day: | 14.24425649 |
| mean anomaly at epoch: | 146.5021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|