View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00053U 60009E 23036.74110831 -.00000045 00000-0 40005-3 0 9994
2 00053 47.2748 168.2795 0098751 48.8407 312.0851 12.17289649785909
| Epoch (UTC): | 05 February 2023 17:47:11 |
| Eccentricity: | 0.0098751 |
| inclination: | 47.2748° |
| perigee height: | 1525 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 168.2795° |
| argument of perigee: | 48.8407° |
| revolutions per day: | 12.17289649 |
| mean anomaly at epoch: | 312.0851° |
| orbit number at epoch: | 78590 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|