View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58793U 26145.55136708 +.00000000 +00000-0 +59359-4 0 00003
2 58793 43.0006 90.9469 0000507 248.4245 111.6552 15.27577403 07
| Epoch (UTC): | 25 May 2026 13:13:58 |
| Eccentricity: | 0.0000507 |
| inclination: | 43.0006° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 90.9469° |
| argument of perigee: | 248.4245° |
| revolutions per day: | 15.27577403 |
| mean anomaly at epoch: | 111.6552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|