View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57513U 26145.48786310 +.00000000 +00000-0 +20333-4 0 00004
2 57513 43.0036 302.0593 0001404 279.6628 80.4065 15.27576058 09
| Epoch (UTC): | 25 May 2026 11:42:31 |
| Eccentricity: | 0.0001404 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.0593° |
| argument of perigee: | 279.6628° |
| revolutions per day: | 15.27576058 |
| mean anomaly at epoch: | 80.4065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|