View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40364U 26145.58936178 +.00000000 +00000-0 +00000-0 0 00005
2 40364 0.0565 24.5491 0004955 34.3211 64.6620 1.00272000 03
| Epoch (UTC): | 25 May 2026 14:08:40 |
| Eccentricity: | 0.0004955 |
| inclination: | 0.0565° |
| perigee height: | 35766 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 24.5491° |
| argument of perigee: | 34.3211° |
| revolutions per day: | 1.00272000 |
| mean anomaly at epoch: | 64.6620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|