View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40018U 26106.37308841 +.00000000 +00000-0 +53351-4 0 00006
2 40018 97.8958 241.1173 0067049 40.0434 320.5690 14.74145358 08
| Epoch (UTC): | 16 April 2026 08:57:14 |
| Eccentricity: | 0.0067049 |
| inclination: | 97.8958° |
| perigee height: | 601 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 241.1173° |
| argument of perigee: | 40.0434° |
| revolutions per day: | 14.74145358 |
| mean anomaly at epoch: | 320.5690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|