View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65520U 26145.62466370 +.00000000 +00000-0 +45466-3 0 00001
2 65520 97.4463 215.1941 0002335 144.7706 215.3676 15.05658080 06
| Epoch (UTC): | 25 May 2026 14:59:30 |
| Eccentricity: | 0.0002335 |
| inclination: | 97.4463° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 215.1941° |
| argument of perigee: | 144.7706° |
| revolutions per day: | 15.05658080 |
| mean anomaly at epoch: | 215.3676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|