View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55628U 26145.04668904 +.00000000 +00000-0 +39433-4 0 00000
2 55628 69.9998 12.0208 0002829 269.6302 90.4533 14.98330512 00
| Epoch (UTC): | 25 May 2026 01:07:13 |
| Eccentricity: | 0.0002829 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 12.0208° |
| argument of perigee: | 269.6302° |
| revolutions per day: | 14.98330512 |
| mean anomaly at epoch: | 90.4533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|