View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55765U 26145.42662497 +.00000000 +00000-0 -62726-4 0 00007
2 55765 70.0000 31.1356 0002564 267.4673 92.6193 14.98333291 01
| Epoch (UTC): | 25 May 2026 10:14:20 |
| Eccentricity: | 0.0002564 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.1356° |
| argument of perigee: | 267.4673° |
| revolutions per day: | 14.98333291 |
| mean anomaly at epoch: | 92.6193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|