View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45582U 26145.22222102 +.00000000 +00000-0 +50841-3 0 00009
2 45582 53.0475 45.8123 0006879 69.3057 290.8697 15.72152160 04
| Epoch (UTC): | 25 May 2026 05:19:59 |
| Eccentricity: | 0.0006879 |
| inclination: | 53.0475° |
| perigee height: | 348 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 45.8123° |
| argument of perigee: | 69.3057° |
| revolutions per day: | 15.72152160 |
| mean anomaly at epoch: | 290.8697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|