View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32382U 26145.57716715 +.00000000 +00000-0 +49800-4 0 00003
2 32382 98.5787 152.8331 0001285 83.6967 276.4362 14.29982931 00
| Epoch (UTC): | 25 May 2026 13:51:07 |
| Eccentricity: | 0.0001285 |
| inclination: | 98.5787° |
| perigee height: | 791 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 152.8331° |
| argument of perigee: | 83.6967° |
| revolutions per day: | 14.29982931 |
| mean anomaly at epoch: | 276.4362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|