View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55643U 26145.30933201 +.00000000 +00000-0 -38786-5 0 00003
2 55643 69.9998 351.4525 0002855 268.7706 91.3126 14.98328626 07
| Epoch (UTC): | 25 May 2026 07:25:26 |
| Eccentricity: | 0.0002855 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 351.4525° |
| argument of perigee: | 268.7706° |
| revolutions per day: | 14.98328626 |
| mean anomaly at epoch: | 91.3126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|