View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45538U 26145.20756000 +.00000000 +00000-0 -29738-2 0 00008
2 45538 53.1577 104.1896 0003324 102.2364 257.9012 15.35599058 00
| Epoch (UTC): | 25 May 2026 04:58:53 |
| Eccentricity: | 0.0003324 |
| inclination: | 53.1577° |
| perigee height: | 457 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 104.1896° |
| argument of perigee: | 102.2364° |
| revolutions per day: | 15.35599058 |
| mean anomaly at epoch: | 257.9012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|