View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63322U 26145.46941148 +.00000000 +00000-0 +51768-3 0 00004
2 63322 42.9998 316.9126 0001360 258.9530 101.1169 15.27592804 01
| Epoch (UTC): | 25 May 2026 11:15:57 |
| Eccentricity: | 0.0001360 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.9126° |
| argument of perigee: | 258.9530° |
| revolutions per day: | 15.27592804 |
| mean anomaly at epoch: | 101.1169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|