View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66278U 26145.38092478 +.00000000 +00000-0 +23941-3 0 00003
2 66278 53.1588 193.9275 0001334 84.1239 275.9915 15.34396248 08
| Epoch (UTC): | 25 May 2026 09:08:31 |
| Eccentricity: | 0.0001334 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 193.9275° |
| argument of perigee: | 84.1239° |
| revolutions per day: | 15.34396248 |
| mean anomaly at epoch: | 275.9915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|