View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68130U 26145.36641249 +.00000000 +00000-0 +78213-4 0 00009
2 68130 50.0011 138.1626 0000243 356.8583 3.2287 13.29330592 00
| Epoch (UTC): | 25 May 2026 08:47:38 |
| Eccentricity: | 0.0000243 |
| inclination: | 50.0011° |
| perigee height: | 1149 km |
| apogee height: | 1149 km |
| right ascension of ascending node: | 138.1626° |
| argument of perigee: | 356.8583° |
| revolutions per day: | 13.29330592 |
| mean anomaly at epoch: | 3.2287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|