View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61543U 26145.46876036 +.00000000 +00000-0 -75346-5 0 00001
2 61543 53.1594 217.9644 0000869 75.2990 284.8125 15.69694212 01
| Epoch (UTC): | 25 May 2026 11:15:00 |
| Eccentricity: | 0.0000869 |
| inclination: | 53.1594° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 217.9644° |
| argument of perigee: | 75.2990° |
| revolutions per day: | 15.69694212 |
| mean anomaly at epoch: | 284.8125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|