View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00976U 64064C 22148.33235038 .00000210 00000-0 11919-3 0 9993
2 00976 79.3152 264.8851 0117470 343.5495 16.1866 14.05350440934840
| Epoch (UTC): | 28 May 2022 07:58:35 |
| Eccentricity: | 0.0117470 |
| inclination: | 79.3152° |
| perigee height: | 790 km |
| apogee height: | 960 km |
| right ascension of ascending node: | 264.8851° |
| argument of perigee: | 343.5495° |
| revolutions per day: | 14.05350440 |
| mean anomaly at epoch: | 16.1866° |
| orbit number at epoch: | 93484 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|