View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45590U 26145.52896507 +.00000000 +00000-0 +10363-2 0 00001
2 45590 53.0463 84.1164 0004931 47.8732 312.2697 15.56611913 06
| Epoch (UTC): | 25 May 2026 12:41:42 |
| Eccentricity: | 0.0004931 |
| inclination: | 53.0463° |
| perigee height: | 394 km |
| apogee height: | 401 km |
| right ascension of ascending node: | 84.1164° |
| argument of perigee: | 47.8732° |
| revolutions per day: | 15.56611913 |
| mean anomaly at epoch: | 312.2697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|