View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59429U 26145.11330958 +.00000000 +00000-0 +79072-5 0 00000
2 59429 53.1604 288.5841 0000670 108.4194 251.6880 15.30186204 06
| Epoch (UTC): | 25 May 2026 02:43:09 |
| Eccentricity: | 0.0000670 |
| inclination: | 53.1604° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 288.5841° |
| argument of perigee: | 108.4194° |
| revolutions per day: | 15.30186204 |
| mean anomaly at epoch: | 251.6880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|