View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56840U 26145.66668980 +.00000000 +00000-0 +24288-2 0 00009
2 56840 43.0032 217.6529 0002046 282.0677 172.0262 15.27552414 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0002046 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 217.6529° |
| argument of perigee: | 282.0677° |
| revolutions per day: | 15.27552414 |
| mean anomaly at epoch: | 172.0262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|