View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 36416U 26065.06991316 +.00000000 +00000-0 +35260-3 0 00006
2 36416 63.3895 324.2284 0689792 2.6202 357.8161 13.72967613 00
| Epoch (UTC): | 06 March 2026 01:40:40 |
| Eccentricity: | 0.0689792 |
| inclination: | 63.3895° |
| perigee height: | 481 km |
| apogee height: | 1497 km |
| right ascension of ascending node: | 324.2284° |
| argument of perigee: | 2.6202° |
| revolutions per day: | 13.72967613 |
| mean anomaly at epoch: | 357.8161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|