View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49194U 26145.29974826 +.00000000 +00000-0 -33954-4 0 00004
2 49194 87.9161 340.0144 0001873 86.5776 273.5570 13.18686006 03
| Epoch (UTC): | 25 May 2026 07:11:38 |
| Eccentricity: | 0.0001873 |
| inclination: | 87.9161° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0144° |
| argument of perigee: | 86.5776° |
| revolutions per day: | 13.18686006 |
| mean anomaly at epoch: | 273.5570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|