View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16682U 26071.59632589 +.00000000 +00000-0 +94896-4 0 00009
2 16682 74.0241 123.6837 0013350 44.5031 72.3319 14.37306575 08
| Epoch (UTC): | 12 March 2026 14:18:42 |
| Eccentricity: | 0.0013350 |
| inclination: | 74.0241° |
| perigee height: | 758 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 123.6837° |
| argument of perigee: | 44.5031° |
| revolutions per day: | 14.37306575 |
| mean anomaly at epoch: | 72.3319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|