View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47226U 26146.13407080 +.00000000 +00000-0 +84382-4 0 00005
2 47226 97.8585 221.1899 0001595 90.6401 269.4996 14.84885695 00
| Epoch (UTC): | 26 May 2026 03:13:03 |
| Eccentricity: | 0.0001595 |
| inclination: | 97.8585° |
| perigee height: | 613 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 221.1899° |
| argument of perigee: | 90.6401° |
| revolutions per day: | 14.84885695 |
| mean anomaly at epoch: | 269.4996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|