View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53431U 26145.22513910 +.00000000 +00000-0 -52595-4 0 00001
2 53431 53.2130 120.1505 0001297 100.7718 259.3420 15.08845678 06
| Epoch (UTC): | 25 May 2026 05:24:12 |
| Eccentricity: | 0.0001297 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 120.1505° |
| argument of perigee: | 100.7718° |
| revolutions per day: | 15.08845678 |
| mean anomaly at epoch: | 259.3420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|