View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63445U 26145.28284207 +.00000000 +00000-0 +74207-3 0 00009
2 63445 53.1577 144.4242 0000968 83.5934 276.5182 15.42187543 09
| Epoch (UTC): | 25 May 2026 06:47:17 |
| Eccentricity: | 0.0000968 |
| inclination: | 53.1577° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 144.4242° |
| argument of perigee: | 83.5934° |
| revolutions per day: | 15.42187543 |
| mean anomaly at epoch: | 276.5182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|