View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66671U 26145.16426007 +.00000000 +00000-0 +49950-3 0 00003
2 66671 97.4213 219.2598 0007237 86.3759 273.8304 15.21038368 01
| Epoch (UTC): | 25 May 2026 03:56:32 |
| Eccentricity: | 0.0007237 |
| inclination: | 97.4213° |
| perigee height: | 498 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 219.2598° |
| argument of perigee: | 86.3759° |
| revolutions per day: | 15.21038368 |
| mean anomaly at epoch: | 273.8304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|