View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15773U 26088.22199550 +.00000000 +00000-0 +88481-4 0 00006
2 15773 66.5867 137.5670 0040596 287.4917 132.3039 14.28119984 02
| Epoch (UTC): | 29 March 2026 05:19:40 |
| Eccentricity: | 0.0040596 |
| inclination: | 66.5867° |
| perigee height: | 769 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 137.5670° |
| argument of perigee: | 287.4917° |
| revolutions per day: | 14.28119984 |
| mean anomaly at epoch: | 132.3039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|