View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39728U 26145.59534182 +.00000000 +00000-0 +00000-0 0 00007
2 39728 0.0485 84.5784 0000250 13.4135 58.0142 1.00272710 08
| Epoch (UTC): | 25 May 2026 14:17:17 |
| Eccentricity: | 0.0000250 |
| inclination: | 0.0485° |
| perigee height: | 35785 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 84.5784° |
| argument of perigee: | 13.4135° |
| revolutions per day: | 1.00272710 |
| mean anomaly at epoch: | 58.0142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|