View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43578U 26145.32215808 +.00000000 +00000-0 +44795-5 0 00001
2 43578 86.3967 66.2654 0002300 86.7194 273.4265 14.34217948 09
| Epoch (UTC): | 25 May 2026 07:43:54 |
| Eccentricity: | 0.0002300 |
| inclination: | 86.3967° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 66.2654° |
| argument of perigee: | 86.7194° |
| revolutions per day: | 14.34217948 |
| mean anomaly at epoch: | 273.4265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|