View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55618U 26145.66753030 +.00000000 +00000-0 +26708-4 0 00003
2 55618 43.0016 279.3636 0001200 271.6975 88.3739 15.27580712 03
| Epoch (UTC): | 25 May 2026 16:01:14 |
| Eccentricity: | 0.0001200 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 279.3636° |
| argument of perigee: | 271.6975° |
| revolutions per day: | 15.27580712 |
| mean anomaly at epoch: | 88.3739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|