View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40043U 26074.18355962 +.00000000 +00000-0 +27544-3 0 00007
2 40043 97.7684 226.4448 0049963 24.5891 335.7690 14.84758376 00
| Epoch (UTC): | 15 March 2026 04:24:19 |
| Eccentricity: | 0.0049963 |
| inclination: | 97.7684° |
| perigee height: | 579 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 226.4448° |
| argument of perigee: | 24.5891° |
| revolutions per day: | 14.84758376 |
| mean anomaly at epoch: | 335.7690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|