View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65267U 26145.47797872 +.00000000 +00000-0 +19145-3 0 00001
2 65267 96.5883 77.1303 0003681 190.4049 169.7154 15.96445196 06
| Epoch (UTC): | 25 May 2026 11:28:17 |
| Eccentricity: | 0.0003681 |
| inclination: | 96.5883° |
| perigee height: | 282 km |
| apogee height: | 287 km |
| right ascension of ascending node: | 77.1303° |
| argument of perigee: | 190.4049° |
| revolutions per day: | 15.96445196 |
| mean anomaly at epoch: | 169.7154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|