View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44457U 26145.58615512 +.00000000 +00000-0 +00000-0 0 00008
2 44457 0.0389 111.1714 0000594 37.5026 317.5209 1.00270029 01
| Epoch (UTC): | 25 May 2026 14:04:03 |
| Eccentricity: | 0.0000594 |
| inclination: | 0.0389° |
| perigee height: | 35785 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 111.1714° |
| argument of perigee: | 37.5026° |
| revolutions per day: | 1.00270029 |
| mean anomaly at epoch: | 317.5209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|