View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40544U 26108.96800588 +.00000000 +00000-0 +00000-0 0 00001
2 40544 56.8049 343.2111 0002470 321.1658 38.8691 1.70475771 09
| Epoch (UTC): | 18 April 2026 23:13:55 |
| Eccentricity: | 0.0002470 |
| inclination: | 56.8049° |
| perigee height: | 23215 km |
| apogee height: | 23229 km |
| right ascension of ascending node: | 343.2111° |
| argument of perigee: | 321.1658° |
| revolutions per day: | 1.70475771 |
| mean anomaly at epoch: | 38.8691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|