View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54027U 26145.41556667 +.00000000 +00000-0 +00000-0 0 00009
2 54027 0.0114 293.4827 0001779 134.3021 195.8226 1.00273159 00
| Epoch (UTC): | 25 May 2026 09:58:24 |
| Eccentricity: | 0.0001779 |
| inclination: | 0.0114° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 293.4827° |
| argument of perigee: | 134.3021° |
| revolutions per day: | 1.00273159 |
| mean anomaly at epoch: | 195.8226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|