View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48408U 26145.55202713 +.00000000 +00000-0 +79215-4 0 00008
2 48408 53.1605 335.6634 0001683 83.5379 276.5814 15.31701456 05
| Epoch (UTC): | 25 May 2026 13:14:55 |
| Eccentricity: | 0.0001683 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 335.6634° |
| argument of perigee: | 83.5379° |
| revolutions per day: | 15.31701456 |
| mean anomaly at epoch: | 276.5814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|