View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53552U 26145.50488279 +.00000000 +00000-0 +51317-3 0 00004
2 53552 53.2131 79.2837 0001445 99.9765 260.1390 15.08795588 09
| Epoch (UTC): | 25 May 2026 12:07:01 |
| Eccentricity: | 0.0001445 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 79.2837° |
| argument of perigee: | 99.9765° |
| revolutions per day: | 15.08795588 |
| mean anomaly at epoch: | 260.1390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|