View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37748U 26145.56336167 +.00000000 +00000-0 +00000-0 0 00007
2 37748 1.2704 83.3201 0002902 335.2566 284.3905 1.00272587 08
| Epoch (UTC): | 25 May 2026 13:31:14 |
| Eccentricity: | 0.0002902 |
| inclination: | 1.2704° |
| perigee height: | 35774 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 83.3201° |
| argument of perigee: | 335.2566° |
| revolutions per day: | 1.00272587 |
| mean anomaly at epoch: | 284.3905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|