View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53553U 26145.23253080 +.00000000 +00000-0 +60417-4 0 00007
2 53553 53.2127 80.3805 0001350 67.7788 292.3348 15.08837329 06
| Epoch (UTC): | 25 May 2026 05:34:50 |
| Eccentricity: | 0.0001350 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 80.3805° |
| argument of perigee: | 67.7788° |
| revolutions per day: | 15.08837329 |
| mean anomaly at epoch: | 292.3348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|