View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28647U 05016B 23156.13848699 .00005126 00000-0 27538-3 0 9996
2 28647 56.9938 147.4854 0107908 303.5737 55.5036 15.11702156223229
| Epoch (UTC): | 05 June 2023 03:19:25 |
| Eccentricity: | 0.0107908 |
| inclination: | 56.9938° |
| perigee height: | 456 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 147.4854° |
| argument of perigee: | 303.5737° |
| revolutions per day: | 15.11702156 |
| mean anomaly at epoch: | 55.5036° |
| orbit number at epoch: | 22322 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|