View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59027U 26145.19688051 +.00000000 +00000-0 +38975-4 0 00008
2 59027 43.0027 315.3930 0001702 269.5371 90.5285 15.27576455 04
| Epoch (UTC): | 25 May 2026 04:43:30 |
| Eccentricity: | 0.0001702 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 315.3930° |
| argument of perigee: | 269.5371° |
| revolutions per day: | 15.27576455 |
| mean anomaly at epoch: | 90.5285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|