View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22236U 26100.20223852 +.00000000 +00000-0 +18363-3 0 00005
2 22236 82.5023 248.8858 0015715 87.6127 272.6894 14.96347383 06
| Epoch (UTC): | 10 April 2026 04:51:13 |
| Eccentricity: | 0.0015715 |
| inclination: | 82.5023° |
| perigee height: | 567 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 248.8858° |
| argument of perigee: | 87.6127° |
| revolutions per day: | 14.96347383 |
| mean anomaly at epoch: | 272.6894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|