View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 14064U 83044A 23150.02334014 .00002722 00000-0 20293-3 0 9994
2 14064 65.0005 25.1876 0108614 264.5087 94.3635 15.00546449 48206
| Epoch (UTC): | 30 May 2023 00:33:36 |
| Eccentricity: | 0.0108614 |
| inclination: | 65.0005° |
| perigee height: | 490 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 25.1876° |
| argument of perigee: | 264.5087° |
| revolutions per day: | 15.00546449 |
| mean anomaly at epoch: | 94.3635° |
| orbit number at epoch: | 4820 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|