View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46060U 26145.21289557 +.00000000 +00000-0 -26201-4 0 00002
2 46060 53.1586 118.6729 0000906 81.8124 278.2979 15.30177323 05
| Epoch (UTC): | 25 May 2026 05:06:34 |
| Eccentricity: | 0.0000906 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 118.6729° |
| argument of perigee: | 81.8124° |
| revolutions per day: | 15.30177323 |
| mean anomaly at epoch: | 278.2979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|