View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20301U 88102J 22228.27093059 .00000266 00000-0 16447-3 0 9995
2 20301 70.9977 82.7123 0014051 120.5414 239.7097 14.14150515707264
| Epoch (UTC): | 16 August 2022 06:30:08 |
| Eccentricity: | 0.0014051 |
| inclination: | 70.9977° |
| perigee height: | 835 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 82.7123° |
| argument of perigee: | 120.5414° |
| revolutions per day: | 14.14150515 |
| mean anomaly at epoch: | 239.7097° |
| orbit number at epoch: | 70726 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|