View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32376U 07059A 23153.54541418 .00000609 00000-0 83041-4 0 9993
2 32376 97.8882 337.2341 0001325 93.8887 266.2478 14.82165340837481
| Epoch (UTC): | 02 June 2023 13:05:23 |
| Eccentricity: | 0.0001325 |
| inclination: | 97.8882° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 337.2341° |
| argument of perigee: | 93.8887° |
| revolutions per day: | 14.82165340 |
| mean anomaly at epoch: | 266.2478° |
| orbit number at epoch: | 83748 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|