View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55664U 26144.93774257 +.00000000 +00000-0 +47385-4 0 00001
2 55664 69.9995 332.2919 0002907 268.6667 91.4159 14.98330160 07
| Epoch (UTC): | 24 May 2026 22:30:20 |
| Eccentricity: | 0.0002907 |
| inclination: | 69.9995° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 332.2919° |
| argument of perigee: | 268.6667° |
| revolutions per day: | 14.98330160 |
| mean anomaly at epoch: | 91.4159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|