View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62746U 26145.52205549 +.00000000 +00000-0 +76723-3 0 00006
2 62746 42.9995 80.8475 0000833 281.2104 78.8654 15.27590354 08
| Epoch (UTC): | 25 May 2026 12:31:45 |
| Eccentricity: | 0.0000833 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.8475° |
| argument of perigee: | 281.2104° |
| revolutions per day: | 15.27590354 |
| mean anomaly at epoch: | 78.8654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|