View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59701U 26145.59917419 +.00000000 +00000-0 -31228-3 0 00008
2 59701 43.0022 345.6207 0000901 287.0244 73.0509 15.27599719 08
| Epoch (UTC): | 25 May 2026 14:22:48 |
| Eccentricity: | 0.0000901 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.6207° |
| argument of perigee: | 287.0244° |
| revolutions per day: | 15.27599719 |
| mean anomaly at epoch: | 73.0509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|