View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 16615U 86019C 24287.06892322 .00001373 00000-0 51883-3 0 9990
2 16615 98.2676 318.4394 0012600 52.0713 328.4613 14.32744169 22213
| Epoch (UTC): | 13 October 2024 01:39:14 |
| Eccentricity: | 0.0012600 |
| inclination: | 98.2676° |
| perigee height: | 773 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 318.4394° |
| argument of perigee: | 52.0713° |
| revolutions per day: | 14.32744169 |
| mean anomaly at epoch: | 328.4613° |
| orbit number at epoch: | 2221 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|