View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55428U 26145.57103448 +.00000000 +00000-0 +74909-4 0 00000
2 55428 69.9993 250.7939 0003533 266.0806 93.9949 14.98331126 09
| Epoch (UTC): | 25 May 2026 13:42:17 |
| Eccentricity: | 0.0003533 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 250.7939° |
| argument of perigee: | 266.0806° |
| revolutions per day: | 14.98331126 |
| mean anomaly at epoch: | 93.9949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|