View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60387U 26145.58685271 +.00000000 +00000-0 +12833-3 0 00007
2 60387 88.9719 282.3395 0018246 86.8523 273.4716 13.51010987 08
| Epoch (UTC): | 25 May 2026 14:05:04 |
| Eccentricity: | 0.0018246 |
| inclination: | 88.9719° |
| perigee height: | 1055 km |
| apogee height: | 1082 km |
| right ascension of ascending node: | 282.3395° |
| argument of perigee: | 86.8523° |
| revolutions per day: | 13.51010987 |
| mean anomaly at epoch: | 273.4716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|