View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42736U 98067MR 19116.58349394 .05344197 12378-4 56382-3 0 9990
2 42736 51.6116 172.4218 0006034 335.7210 140.8917 16.36759636110007
| Epoch (UTC): | 26 April 2019 14:00:13 |
| Eccentricity: | 0.0006034 |
| inclination: | 51.6116° |
| perigee height: | 170 km |
| apogee height: | 178 km |
| right ascension of ascending node: | 172.4218° |
| argument of perigee: | 335.7210° |
| revolutions per day: | 16.36759636 |
| mean anomaly at epoch: | 140.8917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|