View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47265U 26145.56268199 +.00000000 +00000-0 +10835-2 0 00000
2 47265 87.8949 355.1707 0001770 86.6050 273.5281 13.12442166 07
| Epoch (UTC): | 25 May 2026 13:30:15 |
| Eccentricity: | 0.0001770 |
| inclination: | 87.8949° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1707° |
| argument of perigee: | 86.6050° |
| revolutions per day: | 13.12442166 |
| mean anomaly at epoch: | 273.5281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|