View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39159U 26118.84934838 +.00000000 +00000-0 +52356-4 0 00000
2 39159 98.3561 99.8999 0002962 281.6715 78.4132 14.23586221 02
| Epoch (UTC): | 28 April 2026 20:23:03 |
| Eccentricity: | 0.0002962 |
| inclination: | 98.3561° |
| perigee height: | 811 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 99.8999° |
| argument of perigee: | 281.6715° |
| revolutions per day: | 14.23586221 |
| mean anomaly at epoch: | 78.4132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|