View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40069U 26135.27332810 +.00000000 +00000-0 +23419-3 0 00007
2 40069 98.5093 112.1811 0006615 124.2499 235.9307 14.21453398 08
| Epoch (UTC): | 15 May 2026 06:33:35 |
| Eccentricity: | 0.0006615 |
| inclination: | 98.5093° |
| perigee height: | 816 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 112.1811° |
| argument of perigee: | 124.2499° |
| revolutions per day: | 14.21453398 |
| mean anomaly at epoch: | 235.9307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|