View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43880U 26145.55216064 +.00000000 +00000-0 +67103-3 0 00003
2 43880 97.5853 72.9261 0009807 58.2053 302.0148 15.44526568 00
| Epoch (UTC): | 25 May 2026 13:15:06 |
| Eccentricity: | 0.0009807 |
| inclination: | 97.5853° |
| perigee height: | 426 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 72.9261° |
| argument of perigee: | 58.2053° |
| revolutions per day: | 15.44526568 |
| mean anomaly at epoch: | 302.0148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|