View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16728U 26067.59210775 +.00000000 +00000-0 +10609-3 0 00003
2 16728 82.9556 134.1179 0029245 286.7364 182.1406 13.77069822 02
| Epoch (UTC): | 08 March 2026 14:12:38 |
| Eccentricity: | 0.0029245 |
| inclination: | 82.9556° |
| perigee height: | 953 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 134.1179° |
| argument of perigee: | 286.7364° |
| revolutions per day: | 13.77069822 |
| mean anomaly at epoch: | 182.1406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|