View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 33498U 09002G 23078.66747567 .00004187 00000-0 54209-3 0 9999
2 33498 98.1445 340.0812 0011985 83.8058 276.4519 14.81365917762154
| Epoch (UTC): | 19 March 2023 16:01:09 |
| Eccentricity: | 0.0011985 |
| inclination: | 98.1445° |
| perigee height: | 616 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 340.0812° |
| argument of perigee: | 83.8058° |
| revolutions per day: | 14.81365917 |
| mean anomaly at epoch: | 276.4519° |
| orbit number at epoch: | 76215 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|