View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54048U 26144.82892051 +.00000000 +00000-0 +00000-0 0 00006
2 54048 0.0431 294.0197 0001781 67.9908 191.8193 1.00271954 00
| Epoch (UTC): | 24 May 2026 19:53:38 |
| Eccentricity: | 0.0001781 |
| inclination: | 0.0431° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 294.0197° |
| argument of perigee: | 67.9908° |
| revolutions per day: | 1.00271954 |
| mean anomaly at epoch: | 191.8193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|