View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62469U 26144.42316330 +.00000000 +00000-0 +84749-3 0 00004
2 62469 43.0015 126.3500 0001746 252.9736 107.0941 15.70866304 03
| Epoch (UTC): | 24 May 2026 10:09:21 |
| Eccentricity: | 0.0001746 |
| inclination: | 43.0015° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 126.3500° |
| argument of perigee: | 252.9736° |
| revolutions per day: | 15.70866304 |
| mean anomaly at epoch: | 107.0941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|