View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 18586U 26100.46405905 +.00000000 +00000-0 +86741-4 0 00003
2 18586 74.0038 123.0237 0019628 141.7696 218.4854 14.38338750 04
| Epoch (UTC): | 10 April 2026 11:08:14 |
| Eccentricity: | 0.0019628 |
| inclination: | 74.0038° |
| perigee height: | 750 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 123.0237° |
| argument of perigee: | 141.7696° |
| revolutions per day: | 14.38338750 |
| mean anomaly at epoch: | 218.4854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|