View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 31699U 07026B 24287.51920913 .00002589 00000-0 37469-3 0 9992
2 31699 97.4533 320.9367 0340570 101.5538 33.9261 14.44224887911170
| Epoch (UTC): | 13 October 2024 12:27:39 |
| Eccentricity: | 0.0340570 |
| inclination: | 97.4533° |
| perigee height: | 502 km |
| apogee height: | 987 km |
| right ascension of ascending node: | 320.9367° |
| argument of perigee: | 101.5538° |
| revolutions per day: | 14.44224887 |
| mean anomaly at epoch: | 33.9261° |
| orbit number at epoch: | 91117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|