View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63730U 26145.32705655 +.00000000 +00000-0 +16977-3 0 00006
2 63730 51.9013 129.1587 0000305 36.5916 323.5067 14.79929940 01
| Epoch (UTC): | 25 May 2026 07:50:57 |
| Eccentricity: | 0.0000305 |
| inclination: | 51.9013° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 129.1587° |
| argument of perigee: | 36.5916° |
| revolutions per day: | 14.79929940 |
| mean anomaly at epoch: | 323.5067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|