View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60606U 26145.60719279 +.00000000 +00000-0 +00000-0 0 00000
2 60606 1.3705 271.1217 0000668 167.8354 141.0385 1.00269575 08
| Epoch (UTC): | 25 May 2026 14:34:21 |
| Eccentricity: | 0.0000668 |
| inclination: | 1.3705° |
| perigee height: | 35784 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 271.1217° |
| argument of perigee: | 167.8354° |
| revolutions per day: | 1.00269575 |
| mean anomaly at epoch: | 141.0385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|