View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28358U 26145.58346844 +.00000000 +00000-0 +00000-0 0 00009
2 28358 0.0344 58.3773 0000184 110.9270 282.9307 1.00271443 08
| Epoch (UTC): | 25 May 2026 14:00:11 |
| Eccentricity: | 0.0000184 |
| inclination: | 0.0344° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 58.3773° |
| argument of perigee: | 110.9270° |
| revolutions per day: | 1.00271443 |
| mean anomaly at epoch: | 282.9307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|