View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20580U 26096.99605421 +.00000000 +00000-0 +27928-3 0 00008
2 20580 28.4724 206.8372 0002334 83.4383 276.6479 15.29965380 02
| Epoch (UTC): | 06 April 2026 23:54:19 |
| Eccentricity: | 0.0002334 |
| inclination: | 28.4724° |
| perigee height: | 474 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 206.8372° |
| argument of perigee: | 83.4383° |
| revolutions per day: | 15.29965380 |
| mean anomaly at epoch: | 276.6479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|