View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64753U 26145.52901375 +.00000000 +00000-0 +55395-4 0 00009
2 64753 10.9982 114.1650 0003185 219.5428 140.4568 14.29388620 03
| Epoch (UTC): | 25 May 2026 12:41:46 |
| Eccentricity: | 0.0003185 |
| inclination: | 10.9982° |
| perigee height: | 791 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 114.1650° |
| argument of perigee: | 219.5428° |
| revolutions per day: | 14.29388620 |
| mean anomaly at epoch: | 140.4568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|