View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66165U 26145.47033317 +.00000000 +00000-0 +10311-2 0 00001
2 66165 53.1580 65.4729 0001079 70.3847 289.7272 15.34392652 04
| Epoch (UTC): | 25 May 2026 11:17:16 |
| Eccentricity: | 0.0001079 |
| inclination: | 53.1580° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 65.4729° |
| argument of perigee: | 70.3847° |
| revolutions per day: | 15.34392652 |
| mean anomaly at epoch: | 289.7272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|