View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39375U 26145.51938507 +.00000000 +00000-0 +00000-0 0 00006
2 39375 5.9030 72.6385 0001435 269.7172 122.6991 1.00271862 01
| Epoch (UTC): | 25 May 2026 12:27:54 |
| Eccentricity: | 0.0001435 |
| inclination: | 5.9030° |
| perigee height: | 35781 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 72.6385° |
| argument of perigee: | 269.7172° |
| revolutions per day: | 1.00271862 |
| mean anomaly at epoch: | 122.6991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|