View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 51127C 22005Z 24358.18590278 -.00010532 00000+0 -66035-3 0 3581
2 51127 53.2154 121.1156 0001238 91.1276 203.4056 15.08855082 18
| Epoch (UTC): | 23 December 2024 04:27:42 |
| Eccentricity: | 0.0001238 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 121.1156° |
| argument of perigee: | 91.1276° |
| revolutions per day: | 15.08855082 |
| mean anomaly at epoch: | 203.4056° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|