View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 36416U 10009D 23033.51908528 .00000081 00000-0 67220-4 0 9999
2 36416 63.4101 136.5962 0589169 356.9797 2.7740 13.69837009646005
| Epoch (UTC): | 02 February 2023 12:27:28 |
| Eccentricity: | 0.0589169 |
| inclination: | 63.4101° |
| perigee height: | 565 km |
| apogee height: | 1435 km |
| right ascension of ascending node: | 136.5962° |
| argument of perigee: | 356.9797° |
| revolutions per day: | 13.69837009 |
| mean anomaly at epoch: | 2.7740° |
| orbit number at epoch: | 64600 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|