View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63434U 26145.27100455 +.00000000 +00000-0 +50189-3 0 00001
2 63434 53.1576 144.3563 0001109 83.6324 276.4808 15.42169304 02
| Epoch (UTC): | 25 May 2026 06:30:14 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.1576° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 144.3563° |
| argument of perigee: | 83.6324° |
| revolutions per day: | 15.42169304 |
| mean anomaly at epoch: | 276.4808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|