View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65291U 26145.56531929 +.00000000 +00000-0 +19761-3 0 00001
2 65291 97.4465 197.9867 0001523 110.5359 249.6032 15.05655649 04
| Epoch (UTC): | 25 May 2026 13:34:03 |
| Eccentricity: | 0.0001523 |
| inclination: | 97.4465° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 197.9867° |
| argument of perigee: | 110.5359° |
| revolutions per day: | 15.05655649 |
| mean anomaly at epoch: | 249.6032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|