View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65522U 26145.43913921 +.00000000 +00000-0 +30184-3 0 00002
2 65522 97.4455 215.1418 0002522 138.1430 221.9990 15.05654303 03
| Epoch (UTC): | 25 May 2026 10:32:21 |
| Eccentricity: | 0.0002522 |
| inclination: | 97.4455° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 215.1418° |
| argument of perigee: | 138.1430° |
| revolutions per day: | 15.05654303 |
| mean anomaly at epoch: | 221.9990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|