View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20436U 26150.38435360 +.00000000 +00000-0 +20363-3 0 00001
2 20436 98.7117 306.1821 0129642 143.5790 217.4323 14.73865298 09
| Epoch (UTC): | 30 May 2026 09:13:28 |
| Eccentricity: | 0.0129642 |
| inclination: | 98.7117° |
| perigee height: | 558 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 306.1821° |
| argument of perigee: | 143.5790° |
| revolutions per day: | 14.73865298 |
| mean anomaly at epoch: | 217.4323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|