View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 18350U 26105.80441270 +.00000000 +00000-0 +00000-0 0 00000
2 18350 14.4042 351.6879 0006717 8.0624 162.0448 0.98906695 01
| Epoch (UTC): | 15 April 2026 19:18:21 |
| Eccentricity: | 0.0006717 |
| inclination: | 14.4042° |
| perigee height: | 36145 km |
| apogee height: | 36202 km |
| right ascension of ascending node: | 351.6879° |
| argument of perigee: | 8.0624° |
| revolutions per day: | 0.98906695 |
| mean anomaly at epoch: | 162.0448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|