View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47302U 26145.66313007 +.00000000 +00000-0 +75815-4 0 00003
2 47302 98.0447 27.9599 0002689 180.7006 179.4191 14.58858894 00
| Epoch (UTC): | 25 May 2026 15:54:54 |
| Eccentricity: | 0.0002689 |
| inclination: | 98.0447° |
| perigee height: | 695 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 27.9599° |
| argument of perigee: | 180.7006° |
| revolutions per day: | 14.58858894 |
| mean anomaly at epoch: | 179.4191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|