View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00162U 26149.23328176 +.00000000 +00000-0 +59788-4 0 00007
2 00162 47.8990 95.1576 0044310 254.3172 105.2830 14.45387838 07
| Epoch (UTC): | 29 May 2026 05:35:55 |
| Eccentricity: | 0.0044310 |
| inclination: | 47.8990° |
| perigee height: | 709 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 95.1576° |
| argument of perigee: | 254.3172° |
| revolutions per day: | 14.45387838 |
| mean anomaly at epoch: | 105.2830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|