View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27426U 26145.47578338 +.00000000 +00000-0 +00000-0 0 00007
2 27426 4.8223 75.5882 0003356 347.3018 241.3467 1.00272123 05
| Epoch (UTC): | 25 May 2026 11:25:07 |
| Eccentricity: | 0.0003356 |
| inclination: | 4.8223° |
| perigee height: | 35772 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 75.5882° |
| argument of perigee: | 347.3018° |
| revolutions per day: | 1.00272123 |
| mean anomaly at epoch: | 241.3467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|