View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20511U 26020.09558811 +.00000000 +00000-0 +63511-4 0 00009
2 20511 82.5207 268.5187 0014945 250.6170 109.3429 14.82090162 07
| Epoch (UTC): | 20 January 2026 02:17:38 |
| Eccentricity: | 0.0014945 |
| inclination: | 82.5207° |
| perigee height: | 612 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 268.5187° |
| argument of perigee: | 250.6170° |
| revolutions per day: | 14.82090162 |
| mean anomaly at epoch: | 109.3429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|