View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41752U 26145.52709845 +.00000000 +00000-0 +00000-0 0 00000
2 41752 0.1172 87.2837 0010715 190.7463 228.8466 1.00272445 02
| Epoch (UTC): | 25 May 2026 12:39:01 |
| Eccentricity: | 0.0010715 |
| inclination: | 0.1172° |
| perigee height: | 35741 km |
| apogee height: | 35832 km |
| right ascension of ascending node: | 87.2837° |
| argument of perigee: | 190.7463° |
| revolutions per day: | 1.00272445 |
| mean anomaly at epoch: | 228.8466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|