View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 30056U 99025PH 24358.14841414 .00003803 00000-0 30528-2 0 9992
2 30056 98.3519 222.8402 0305254 86.1372 277.4616 13.71585126891221
| Epoch (UTC): | 23 December 2024 03:33:42 |
| Eccentricity: | 0.0305254 |
| inclination: | 98.3519° |
| perigee height: | 769 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 222.8402° |
| argument of perigee: | 86.1372° |
| revolutions per day: | 13.71585126 |
| mean anomaly at epoch: | 277.4616° |
| orbit number at epoch: | 89122 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|