View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40069U 26073.25882351 +.00000000 +00000-0 +22371-3 0 00002
2 40069 98.5032 52.4039 0005121 323.6492 36.4338 14.21432220 07
| Epoch (UTC): | 14 March 2026 06:12:42 |
| Eccentricity: | 0.0005121 |
| inclination: | 98.5032° |
| perigee height: | 817 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 52.4039° |
| argument of perigee: | 323.6492° |
| revolutions per day: | 14.21432220 |
| mean anomaly at epoch: | 36.4338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|