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 23150.11393508 .00000265 00000-0 85481-4 0 9993
2 06324 74.0792 38.1999 0009236 331.3886 28.6763 14.43931361648844
| Epoch (UTC): | 30 May 2023 02:44:03 |
| Eccentricity: | 0.0009236 |
| inclination: | 74.0792° |
| perigee height: | 739 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 38.1999° |
| argument of perigee: | 331.3886° |
| revolutions per day: | 14.43931361 |
| mean anomaly at epoch: | 28.6763° |
| orbit number at epoch: | 64884 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|