View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56728U 26145.31564219 +.00000000 +00000-0 +11557-3 0 00002
2 56728 86.6113 3.2544 0002609 87.4960 272.6555 14.72254973 00
| Epoch (UTC): | 25 May 2026 07:34:31 |
| Eccentricity: | 0.0002609 |
| inclination: | 86.6113° |
| perigee height: | 652 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 3.2544° |
| argument of perigee: | 87.4960° |
| revolutions per day: | 14.72254973 |
| mean anomaly at epoch: | 272.6555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|