View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25544U 26039.85811588 +.00000000 +00000-0 +18006-3 0 00005
2 25544 51.6313 214.8819 0011069 77.9921 282.2307 15.48490499 03
| Epoch (UTC): | 08 February 2026 20:35:41 |
| Eccentricity: | 0.0011069 |
| inclination: | 51.6313° |
| perigee height: | 414 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 214.8819° |
| argument of perigee: | 77.9921° |
| revolutions per day: | 15.48490499 |
| mean anomaly at epoch: | 282.2307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|