View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20442U 26141.32093881 +.00000000 +00000-0 +39650-4 0 00000
2 20442 98.8864 162.3846 0010460 286.7131 73.2904 14.34113811 08
| Epoch (UTC): | 21 May 2026 07:42:09 |
| Eccentricity: | 0.0010460 |
| inclination: | 98.8864° |
| perigee height: | 771 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 162.3846° |
| argument of perigee: | 286.7131° |
| revolutions per day: | 14.34113811 |
| mean anomaly at epoch: | 73.2904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|