View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58956U 26145.46557828 +.00000000 +00000-0 +20712-3 0 00004
2 58956 39.9884 148.8221 0013976 110.8965 249.3279 13.70381835 03
| Epoch (UTC): | 25 May 2026 11:10:25 |
| Eccentricity: | 0.0013976 |
| inclination: | 39.9884° |
| perigee height: | 988 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 148.8221° |
| argument of perigee: | 110.8965° |
| revolutions per day: | 13.70381835 |
| mean anomaly at epoch: | 249.3279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|