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 23332.49060354 .00000132 00000-0 15955-3 0 9999
2 00116 66.8109 10.0194 0078957 210.7519 148.8923 13.91972464167012
| Epoch (UTC): | 28 November 2023 11:46:28 |
| Eccentricity: | 0.0078957 |
| inclination: | 66.8109° |
| perigee height: | 864 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 10.0194° |
| argument of perigee: | 210.7519° |
| revolutions per day: | 13.91972464 |
| mean anomaly at epoch: | 148.8923° |
| orbit number at epoch: | 16701 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|