View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49190U 26145.47511087 +.00000000 +00000-0 +59542-4 0 00006
2 49190 87.9160 339.9841 0001785 87.9514 272.1822 13.18686938 05
| Epoch (UTC): | 25 May 2026 11:24:09 |
| Eccentricity: | 0.0001785 |
| inclination: | 87.9160° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9841° |
| argument of perigee: | 87.9514° |
| revolutions per day: | 13.18686938 |
| mean anomaly at epoch: | 272.1822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|