View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57641U 26145.66166494 +.00000000 +00000-0 +17284-3 0 00001
2 57641 42.9998 17.3934 0001238 267.5770 92.4940 15.27592674 07
| Epoch (UTC): | 25 May 2026 15:52:47 |
| Eccentricity: | 0.0001238 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 17.3934° |
| argument of perigee: | 267.5770° |
| revolutions per day: | 15.27592674 |
| mean anomaly at epoch: | 92.4940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|