View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66957U 26145.37159701 +.00000000 +00000-0 +72922-4 0 00003
2 66957 86.4906 290.0414 0001548 110.6020 249.5280 13.24411573 07
| Epoch (UTC): | 25 May 2026 08:55:05 |
| Eccentricity: | 0.0001548 |
| inclination: | 86.4906° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 290.0414° |
| argument of perigee: | 110.6020° |
| revolutions per day: | 13.24411573 |
| mean anomaly at epoch: | 249.5280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|