View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 16495U 86006A 24304.11768317 .17852326 -10704-5 22495-3 0 9999
2 16495 82.4314 217.1065 0008201 211.1251 248.8719 16.49433626128289
| Epoch (UTC): | 30 October 2024 02:49:27 |
| Eccentricity: | 0.0008201 |
| inclination: | 82.4314° |
| perigee height: | 135 km |
| apogee height: | 146 km |
| right ascension of ascending node: | 217.1065° |
| argument of perigee: | 211.1251° |
| revolutions per day: | 16.49433626 |
| mean anomaly at epoch: | 248.8719° |
| orbit number at epoch: | 12828 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|