View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40351U 26145.23849602 +.00000000 +00000-0 +00000-0 0 00008
2 40351 0.0577 356.4132 0002706 65.3887 298.2249 5.00115986 01
| Epoch (UTC): | 25 May 2026 05:43:26 |
| Eccentricity: | 0.0002706 |
| inclination: | 0.0577° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 356.4132° |
| argument of perigee: | 65.3887° |
| revolutions per day: | 5.00115986 |
| mean anomaly at epoch: | 298.2249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|