View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20580U 26087.79815184 +.00000000 +00000-0 +29315-3 0 00007
2 20580 28.4720 269.6203 0001691 350.4608 9.5956 15.29774056 01
| Epoch (UTC): | 28 March 2026 19:09:20 |
| Eccentricity: | 0.0001691 |
| inclination: | 28.4720° |
| perigee height: | 475 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 269.6203° |
| argument of perigee: | 350.4608° |
| revolutions per day: | 15.29774056 |
| mean anomaly at epoch: | 9.5956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|