View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57680U 26145.55562691 +.00000000 +00000-0 -22429-4 0 00000
2 57680 53.1598 209.9522 0001023 128.6909 231.4183 15.30210903 05
| Epoch (UTC): | 25 May 2026 13:20:06 |
| Eccentricity: | 0.0001023 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.9522° |
| argument of perigee: | 128.6909° |
| revolutions per day: | 15.30210903 |
| mean anomaly at epoch: | 231.4183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|