View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58309U 26145.20351981 +.00000000 +00000-0 +49889-3 0 00006
2 58309 97.3877 236.5066 0005590 212.4737 147.6174 15.55087339 07
| Epoch (UTC): | 25 May 2026 04:53:04 |
| Eccentricity: | 0.0005590 |
| inclination: | 97.3877° |
| perigee height: | 398 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 236.5066° |
| argument of perigee: | 212.4737° |
| revolutions per day: | 15.55087339 |
| mean anomaly at epoch: | 147.6174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|