View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39446U 26097.15018294 +.00000000 +00000-0 +42451-3 0 00002
2 39446 97.8639 52.8068 0049081 194.3973 165.5853 14.96482084 06
| Epoch (UTC): | 07 April 2026 03:36:15 |
| Eccentricity: | 0.0049081 |
| inclination: | 97.8639° |
| perigee height: | 544 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 52.8068° |
| argument of perigee: | 194.3973° |
| revolutions per day: | 14.96482084 |
| mean anomaly at epoch: | 165.5853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|