View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19687U 26135.08160894 +.00000000 +00000-0 +00000-0 0 00007
2 19687 13.1324 337.1463 0004835 324.4976 211.7871 0.99666020 04
| Epoch (UTC): | 15 May 2026 01:57:31 |
| Eccentricity: | 0.0004835 |
| inclination: | 13.1324° |
| perigee height: | 35937 km |
| apogee height: | 35978 km |
| right ascension of ascending node: | 337.1463° |
| argument of perigee: | 324.4976° |
| revolutions per day: | 0.99666020 |
| mean anomaly at epoch: | 211.7871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|