View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57441U 26145.59375818 +.00000000 +00000-0 +70455-4 0 00003
2 57441 43.0023 192.3242 0001776 277.0390 83.0259 15.27581458 00
| Epoch (UTC): | 25 May 2026 14:15:00 |
| Eccentricity: | 0.0001776 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 192.3242° |
| argument of perigee: | 277.0390° |
| revolutions per day: | 15.27581458 |
| mean anomaly at epoch: | 83.0259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|