View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14373U 26067.16285573 +.00000000 +00000-0 +77994-4 0 00009
2 14373 82.5408 143.9907 0020337 139.7818 220.4908 14.86232364 06
| Epoch (UTC): | 08 March 2026 03:54:30 |
| Eccentricity: | 0.0020337 |
| inclination: | 82.5408° |
| perigee height: | 596 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 143.9907° |
| argument of perigee: | 139.7818° |
| revolutions per day: | 14.86232364 |
| mean anomaly at epoch: | 220.4908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|