View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63449U 26145.28255606 +.00000000 +00000-0 +78822-3 0 00001
2 63449 53.1581 144.4094 0000974 77.7125 282.3990 15.42185957 06
| Epoch (UTC): | 25 May 2026 06:46:52 |
| Eccentricity: | 0.0000974 |
| inclination: | 53.1581° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 144.4094° |
| argument of perigee: | 77.7125° |
| revolutions per day: | 15.42185957 |
| mean anomaly at epoch: | 282.3990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|