View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43470U 18045A 18140.97000001 -.00010094 +00000-0 +00000-0 0 9992
2 43470 027.5020 209.5210 9658153 171.2240 002.0960 00.09844104000017
| Epoch (UTC): | 20 May 2018 23:16:48 |
| Eccentricity: | 0.9658153 |
| inclination: | 27.5020° |
| perigee height: | 395 km |
| apogee height: | 383105 km |
| right ascension of ascending node: | 209.5210° |
| argument of perigee: | 171.2240° |
| revolutions per day: | 0.09844104 |
| mean anomaly at epoch: | 2.0960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|