View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61788U 26145.61324406 +.00000000 +00000-0 +61653-3 0 00001
2 61788 97.2934 20.9267 0007319 29.6328 330.5340 15.55935749 03
| Epoch (UTC): | 25 May 2026 14:43:04 |
| Eccentricity: | 0.0007319 |
| inclination: | 97.2934° |
| perigee height: | 394 km |
| apogee height: | 404 km |
| right ascension of ascending node: | 20.9267° |
| argument of perigee: | 29.6328° |
| revolutions per day: | 15.55935749 |
| mean anomaly at epoch: | 330.5340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|