View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59739U 26145.38756093 +.00000000 +00000-0 +37199-3 0 00007
2 59739 42.9994 110.0403 0000869 246.7325 113.3435 15.27584984 06
| Epoch (UTC): | 25 May 2026 09:18:05 |
| Eccentricity: | 0.0000869 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.0403° |
| argument of perigee: | 246.7325° |
| revolutions per day: | 15.27584984 |
| mean anomaly at epoch: | 113.3435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|