View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59750U 26145.30816620 +.00000000 +00000-0 +84480-4 0 00001
2 59750 43.0030 111.1592 0001210 267.0941 92.9772 15.27583059 02
| Epoch (UTC): | 25 May 2026 07:23:45 |
| Eccentricity: | 0.0001210 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 111.1592° |
| argument of perigee: | 267.0941° |
| revolutions per day: | 15.27583059 |
| mean anomaly at epoch: | 92.9772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|