View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23439U 26109.22643182 +.00000000 +00000-0 -19623-3 0 00005
2 23439 64.8192 38.5703 0154212 14.5898 345.9405 11.27583786 07
| Epoch (UTC): | 19 April 2026 05:26:03 |
| Eccentricity: | 0.0154212 |
| inclination: | 64.8192° |
| perigee height: | 1893 km |
| apogee height: | 2152 km |
| right ascension of ascending node: | 38.5703° |
| argument of perigee: | 14.5898° |
| revolutions per day: | 11.27583786 |
| mean anomaly at epoch: | 345.9405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|