View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43255U 26145.39726071 +.00000000 +00000-0 -19154-4 0 00000
2 43255 86.3936 299.9931 0001990 95.0385 265.1038 14.34218046 05
| Epoch (UTC): | 25 May 2026 09:32:03 |
| Eccentricity: | 0.0001990 |
| inclination: | 86.3936° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 299.9931° |
| argument of perigee: | 95.0385° |
| revolutions per day: | 14.34218046 |
| mean anomaly at epoch: | 265.1038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|