View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68227U 26145.24136786 +.00000000 +00000-0 +42054-3 0 00001
2 68227 97.2867 20.7481 0001603 86.9200 273.2226 15.33455690 08
| Epoch (UTC): | 25 May 2026 05:47:34 |
| Eccentricity: | 0.0001603 |
| inclination: | 97.2867° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.7481° |
| argument of perigee: | 86.9200° |
| revolutions per day: | 15.33455690 |
| mean anomaly at epoch: | 273.2226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|