View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 06324U 72104B 23088.86599850 .00000572 00000-0 17540-3 0 9994
2 06324 74.0773 151.7981 0007728 109.0208 251.1787 14.43866154640004
| Epoch (UTC): | 29 March 2023 20:47:02 |
| Eccentricity: | 0.0007728 |
| inclination: | 74.0773° |
| perigee height: | 740 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 151.7981° |
| argument of perigee: | 109.0208° |
| revolutions per day: | 14.43866154 |
| mean anomaly at epoch: | 251.1787° |
| orbit number at epoch: | 64000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|