View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28353U 26018.60452992 +.00000000 +00000-0 -42057-4 0 00001
2 28353 71.0029 337.6005 0002832 136.8894 223.2450 14.14592511 01
| Epoch (UTC): | 18 January 2026 14:30:31 |
| Eccentricity: | 0.0002832 |
| inclination: | 71.0029° |
| perigee height: | 842 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 337.6005° |
| argument of perigee: | 136.8894° |
| revolutions per day: | 14.14592511 |
| mean anomaly at epoch: | 223.2450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|