View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58239U 26145.46211703 +.00000000 +00000-0 +30026-3 0 00006
2 58239 42.9993 211.8532 0001809 269.1444 90.9201 15.27580961 00
| Epoch (UTC): | 25 May 2026 11:05:26 |
| Eccentricity: | 0.0001809 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.8532° |
| argument of perigee: | 269.1444° |
| revolutions per day: | 15.27580961 |
| mean anomaly at epoch: | 90.9201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|