View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60086U 26145.23107891 +.00000000 +00000-0 +00000-0 0 00002
2 60086 0.0713 32.7295 0001380 278.3825 34.0892 1.00262496 04
| Epoch (UTC): | 25 May 2026 05:32:45 |
| Eccentricity: | 0.0001380 |
| inclination: | 0.0713° |
| perigee height: | 35783 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 32.7295° |
| argument of perigee: | 278.3825° |
| revolutions per day: | 1.00262496 |
| mean anomaly at epoch: | 34.0892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|