View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48274U 26111.49715219 +.00000000 +00000-0 +25250-3 0 00004
2 48274 41.4677 307.2849 0006600 248.2463 111.7674 15.62743674 02
| Epoch (UTC): | 21 April 2026 11:55:53 |
| Eccentricity: | 0.0006600 |
| inclination: | 41.4677° |
| perigee height: | 375 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 307.2849° |
| argument of perigee: | 248.2463° |
| revolutions per day: | 15.62743674 |
| mean anomaly at epoch: | 111.7674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|