View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55750U 26145.15563275 +.00000000 +00000-0 +79341-4 0 00005
2 55750 70.0006 51.6755 0002744 269.1629 90.9215 14.98331346 06
| Epoch (UTC): | 25 May 2026 03:44:06 |
| Eccentricity: | 0.0002744 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 51.6755° |
| argument of perigee: | 269.1629° |
| revolutions per day: | 14.98331346 |
| mean anomaly at epoch: | 90.9215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|