View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00116U 61015A 23338.45420628 .00000080 00000-0 11998-3 0 9990
2 00116 66.8106 355.4352 0078476 206.8019 152.8997 13.91974796167845
| Epoch (UTC): | 04 December 2023 10:54:03 |
| Eccentricity: | 0.0078476 |
| inclination: | 66.8106° |
| perigee height: | 864 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 355.4352° |
| argument of perigee: | 206.8019° |
| revolutions per day: | 13.91974796 |
| mean anomaly at epoch: | 152.8997° |
| orbit number at epoch: | 16784 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|