View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14453U 26071.65733131 +.00000000 +00000-0 +53092-4 0 00008
2 14453 81.1663 135.5193 0103779 190.1813 169.7267 14.25440331 06
| Epoch (UTC): | 12 March 2026 15:46:33 |
| Eccentricity: | 0.0103779 |
| inclination: | 81.1663° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 135.5193° |
| argument of perigee: | 190.1813° |
| revolutions per day: | 14.25440331 |
| mean anomaly at epoch: | 169.7267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|