View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40719U 26118.57519978 +.00000000 +00000-0 +53481-3 0 00007
2 40719 97.5946 336.3574 0014327 48.2509 311.9938 15.03152879 04
| Epoch (UTC): | 28 April 2026 13:48:17 |
| Eccentricity: | 0.0014327 |
| inclination: | 97.5946° |
| perigee height: | 547 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 336.3574° |
| argument of perigee: | 48.2509° |
| revolutions per day: | 15.03152879 |
| mean anomaly at epoch: | 311.9938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|