View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47652U 26145.48344249 +.00000000 +00000-0 +12492-2 0 00003
2 47652 53.1557 57.5774 0007719 94.6354 265.5539 15.54815117 05
| Epoch (UTC): | 25 May 2026 11:36:09 |
| Eccentricity: | 0.0007719 |
| inclination: | 53.1557° |
| perigee height: | 397 km |
| apogee height: | 408 km |
| right ascension of ascending node: | 57.5774° |
| argument of perigee: | 94.6354° |
| revolutions per day: | 15.54815117 |
| mean anomaly at epoch: | 265.5539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|