View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59623U 26145.22755918 +.00000000 +00000-0 +14304-4 0 00001
2 59623 43.0034 326.0494 0001356 276.3324 83.7373 15.27578274 00
| Epoch (UTC): | 25 May 2026 05:27:41 |
| Eccentricity: | 0.0001356 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 326.0494° |
| argument of perigee: | 276.3324° |
| revolutions per day: | 15.27578274 |
| mean anomaly at epoch: | 83.7373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|