View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66308U 26145.56662590 +.00000000 +00000-0 +15898-3 0 00007
2 66308 45.3973 242.4984 0006004 263.1581 96.8622 15.20277341 00
| Epoch (UTC): | 25 May 2026 13:35:56 |
| Eccentricity: | 0.0006004 |
| inclination: | 45.3973° |
| perigee height: | 501 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 242.4984° |
| argument of perigee: | 263.1581° |
| revolutions per day: | 15.20277341 |
| mean anomaly at epoch: | 96.8622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|