View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 51080U 22002DA 23032.91769551 .00013544 00000-0 60184-3 0 9992
2 51080 97.4812 103.9055 0012487 19.9132 340.2588 15.21577921 58279
| Epoch (UTC): | 01 February 2023 22:01:28 |
| Eccentricity: | 0.0012487 |
| inclination: | 97.4812° |
| perigee height: | 492 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 103.9055° |
| argument of perigee: | 19.9132° |
| revolutions per day: | 15.21577921 |
| mean anomaly at epoch: | 340.2588° |
| orbit number at epoch: | 5827 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|