View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27606U 26133.96450484 +.00000000 +00000-0 +50284-4 0 00002
2 27606 64.5552 355.5632 0087177 276.6200 82.4985 14.76978303 06
| Epoch (UTC): | 13 May 2026 23:08:53 |
| Eccentricity: | 0.0087177 |
| inclination: | 64.5552° |
| perigee height: | 578 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 355.5632° |
| argument of perigee: | 276.6200° |
| revolutions per day: | 14.76978303 |
| mean anomaly at epoch: | 82.4985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|