View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37386U 11014A 26010.73681048 0.00000000 00000-0 00000-0 0 03
2 37386 63.4482 323.5944 0348790 356.1535 3.8464 13.41361261 08
| Epoch (UTC): | 10 January 2026 17:41:00 |
| Eccentricity: | 0.0348790 |
| inclination: | 63.4482° |
| perigee height: | 843 km |
| apogee height: | 1365 km |
| right ascension of ascending node: | 323.5944° |
| argument of perigee: | 356.1535° |
| revolutions per day: | 13.41361261 |
| mean anomaly at epoch: | 3.8464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|