View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63433U 26145.39749578 +.00000000 +00000-0 +84642-3 0 00009
2 63433 53.1582 143.7209 0000935 70.3090 289.8017 15.42186919 08
| Epoch (UTC): | 25 May 2026 09:32:23 |
| Eccentricity: | 0.0000935 |
| inclination: | 53.1582° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.7209° |
| argument of perigee: | 70.3090° |
| revolutions per day: | 15.42186919 |
| mean anomaly at epoch: | 289.8017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|