View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63733U 26145.23383134 +.00000000 +00000-0 -19218-3 0 00005
2 63733 51.9029 122.1078 0000415 78.4897 281.6112 14.79931033 05
| Epoch (UTC): | 25 May 2026 05:36:43 |
| Eccentricity: | 0.0000415 |
| inclination: | 51.9029° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 122.1078° |
| argument of perigee: | 78.4897° |
| revolutions per day: | 14.79931033 |
| mean anomaly at epoch: | 281.6112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|