View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44243U 19029J 20287.71504568 .11982673 12791-4 10982-3 0 9997
2 44243 52.9786 228.8138 0008105 330.1078 31.0927 16.50981164 79283
| Epoch (UTC): | 13 October 2020 17:09:39 |
| Eccentricity: | 0.0008105 |
| inclination: | 52.9786° |
| perigee height: | 131 km |
| apogee height: | 142 km |
| right ascension of ascending node: | 228.8138° |
| argument of perigee: | 330.1078° |
| revolutions per day: | 16.50981164 |
| mean anomaly at epoch: | 31.0927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|