View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55841U 26144.45529595 +.00000000 +00000-0 +00000-0 0 00007
2 55841 0.0315 64.1940 0000543 123.6452 280.1163 1.00274145 08
| Epoch (UTC): | 24 May 2026 10:55:37 |
| Eccentricity: | 0.0000543 |
| inclination: | 0.0315° |
| perigee height: | 35784 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 64.1940° |
| argument of perigee: | 123.6452° |
| revolutions per day: | 1.00274145 |
| mean anomaly at epoch: | 280.1163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|