View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42709U 26145.51919816 +.00000000 +00000-0 +00000-0 0 00003
2 42709 0.0194 335.6185 0000545 70.2694 254.9736 1.00270280 07
| Epoch (UTC): | 25 May 2026 12:27:38 |
| Eccentricity: | 0.0000545 |
| inclination: | 0.0194° |
| perigee height: | 35785 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 335.6185° |
| argument of perigee: | 70.2694° |
| revolutions per day: | 1.00270280 |
| mean anomaly at epoch: | 254.9736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|