View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62571U 26145.57910316 +.00000000 +00000-0 +72526-3 0 00009
2 62571 43.0026 218.1949 0001542 278.4317 81.6359 15.27580913 09
| Epoch (UTC): | 25 May 2026 13:53:54 |
| Eccentricity: | 0.0001542 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 218.1949° |
| argument of perigee: | 278.4317° |
| revolutions per day: | 15.27580913 |
| mean anomaly at epoch: | 81.6359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|