View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20663U 26071.77700403 +.00000000 +00000-0 +20542-3 0 00000
2 20663 62.7917 325.0488 0016612 190.8037 169.2709 15.05671456 09
| Epoch (UTC): | 12 March 2026 18:38:53 |
| Eccentricity: | 0.0016612 |
| inclination: | 62.7917° |
| perigee height: | 538 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 325.0488° |
| argument of perigee: | 190.8037° |
| revolutions per day: | 15.05671456 |
| mean anomaly at epoch: | 169.2709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|