View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27606U 02058B 23337.99247028 .00001230 00000-0 20240-3 0 9992
2 27606 64.5547 202.5085 0063616 190.7593 169.2153 14.73862721125435
| Epoch (UTC): | 03 December 2023 23:49:09 |
| Eccentricity: | 0.0063616 |
| inclination: | 64.5547° |
| perigee height: | 604 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 202.5085° |
| argument of perigee: | 190.7593° |
| revolutions per day: | 14.73862721 |
| mean anomaly at epoch: | 169.2153° |
| orbit number at epoch: | 12543 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|