View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47509U 26145.56790068 +.00000000 +00000-0 +15759-3 0 00007
2 47509 97.2168 193.2189 0003579 235.9074 124.1832 15.37488042 00
| Epoch (UTC): | 25 May 2026 13:37:46 |
| Eccentricity: | 0.0003579 |
| inclination: | 97.2168° |
| perigee height: | 451 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 193.2189° |
| argument of perigee: | 235.9074° |
| revolutions per day: | 15.37488042 |
| mean anomaly at epoch: | 124.1832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|