View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 12443U 26072.31156878 +.00000000 +00000-0 +66992-4 0 00009
2 12443 74.0514 84.7594 0003056 128.3372 231.8057 14.36033869 03
| Epoch (UTC): | 13 March 2026 07:28:39 |
| Eccentricity: | 0.0003056 |
| inclination: | 74.0514° |
| perigee height: | 769 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 84.7594° |
| argument of perigee: | 128.3372° |
| revolutions per day: | 14.36033869 |
| mean anomaly at epoch: | 231.8057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|