View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55927U 26145.61962843 +.00000000 +00000-0 +76891-5 0 00004
2 55927 69.9991 110.3652 0003427 266.6149 93.4618 14.98332416 03
| Epoch (UTC): | 25 May 2026 14:52:15 |
| Eccentricity: | 0.0003427 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 110.3652° |
| argument of perigee: | 266.6149° |
| revolutions per day: | 14.98332416 |
| mean anomaly at epoch: | 93.4618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|