View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66728U 26145.46038102 +.00000000 +00000-0 +24399-3 0 00004
2 66728 97.4199 219.5806 0001658 79.2043 280.9379 15.20374454 09
| Epoch (UTC): | 25 May 2026 11:02:56 |
| Eccentricity: | 0.0001658 |
| inclination: | 97.4199° |
| perigee height: | 504 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 219.5806° |
| argument of perigee: | 79.2043° |
| revolutions per day: | 15.20374454 |
| mean anomaly at epoch: | 280.9379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|