View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 18583U 26145.92683788 +.00000000 +00000-0 +00000-0 0 00007
2 18583 12.0752 338.4858 0025918 280.6509 266.0587 0.98388070 05
| Epoch (UTC): | 25 May 2026 22:14:38 |
| Eccentricity: | 0.0025918 |
| inclination: | 12.0752° |
| perigee height: | 36212 km |
| apogee height: | 36434 km |
| right ascension of ascending node: | 338.4858° |
| argument of perigee: | 280.6509° |
| revolutions per day: | 0.98388070 |
| mean anomaly at epoch: | 266.0587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|