View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53011U 26145.14238597 +.00000000 +00000-0 +48284-4 0 00000
2 53011 53.2153 100.9097 0001612 73.9505 286.1664 15.08840553 08
| Epoch (UTC): | 25 May 2026 03:25:02 |
| Eccentricity: | 0.0001612 |
| inclination: | 53.2153° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.9097° |
| argument of perigee: | 73.9505° |
| revolutions per day: | 15.08840553 |
| mean anomaly at epoch: | 286.1664° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|