View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65620U 26145.49466780 +.00000000 +00000-0 +14899-3 0 00008
2 65620 50.0002 81.6887 0005409 326.2463 33.8070 13.41468745 04
| Epoch (UTC): | 25 May 2026 11:52:19 |
| Eccentricity: | 0.0005409 |
| inclination: | 50.0002° |
| perigee height: | 1100 km |
| apogee height: | 1108 km |
| right ascension of ascending node: | 81.6887° |
| argument of perigee: | 326.2463° |
| revolutions per day: | 13.41468745 |
| mean anomaly at epoch: | 33.8070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|