View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27430U 26150.42575131 +.00000000 +00000-0 +14420-3 0 00005
2 27430 98.7278 112.3305 0009586 125.2032 235.0051 14.33140504 08
| Epoch (UTC): | 30 May 2026 10:13:04 |
| Eccentricity: | 0.0009586 |
| inclination: | 98.7278° |
| perigee height: | 774 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 112.3305° |
| argument of perigee: | 125.2032° |
| revolutions per day: | 14.33140504 |
| mean anomaly at epoch: | 235.0051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|