View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63826U 26145.27361339 +.00000000 +00000-0 +55879-3 0 00007
2 63826 43.0025 100.3383 0001364 272.2927 87.7769 15.27594360 00
| Epoch (UTC): | 25 May 2026 06:34:00 |
| Eccentricity: | 0.0001364 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.3383° |
| argument of perigee: | 272.2927° |
| revolutions per day: | 15.27594360 |
| mean anomaly at epoch: | 87.7769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|