View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55771U 26145.66444382 +.00000000 +00000-0 +76091-4 0 00000
2 55771 70.0000 30.3605 0002436 273.8940 86.1940 14.98324794 08
| Epoch (UTC): | 25 May 2026 15:56:47 |
| Eccentricity: | 0.0002436 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 30.3605° |
| argument of perigee: | 273.8940° |
| revolutions per day: | 14.98324794 |
| mean anomaly at epoch: | 86.1940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|