View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66164U 26145.21610191 +.00000000 +00000-0 +10492-2 0 00003
2 66164 53.1593 66.7337 0001026 92.4841 267.6279 15.34413443 01
| Epoch (UTC): | 25 May 2026 05:11:11 |
| Eccentricity: | 0.0001026 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 66.7337° |
| argument of perigee: | 92.4841° |
| revolutions per day: | 15.34413443 |
| mean anomaly at epoch: | 267.6279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|