View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54674U 26145.32136683 +.00000000 +00000-0 +21801-3 0 00004
2 54674 87.9251 248.5270 0001894 102.6201 257.5145 13.21826446 08
| Epoch (UTC): | 25 May 2026 07:42:46 |
| Eccentricity: | 0.0001894 |
| inclination: | 87.9251° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.5270° |
| argument of perigee: | 102.6201° |
| revolutions per day: | 13.21826446 |
| mean anomaly at epoch: | 257.5145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|