View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66400U 26145.49565909 +.00000000 +00000-0 +48237-3 0 00001
2 66400 53.1581 219.4989 0001029 83.0709 277.0410 15.34394633 04
| Epoch (UTC): | 25 May 2026 11:53:44 |
| Eccentricity: | 0.0001029 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.4989° |
| argument of perigee: | 83.0709° |
| revolutions per day: | 15.34394633 |
| mean anomaly at epoch: | 277.0410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|