View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61760U 26145.64151515 +.00000000 +00000-0 +71755-3 0 00007
2 61760 97.2971 23.8515 0003636 28.0399 332.1056 15.64001312 03
| Epoch (UTC): | 25 May 2026 15:23:46 |
| Eccentricity: | 0.0003636 |
| inclination: | 97.2971° |
| perigee height: | 374 km |
| apogee height: | 379 km |
| right ascension of ascending node: | 23.8515° |
| argument of perigee: | 28.0399° |
| revolutions per day: | 15.64001312 |
| mean anomaly at epoch: | 332.1056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|