View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66707U 26145.64437596 +.00000000 +00000-0 +26508-3 0 00005
2 66707 97.4230 219.5628 0006297 86.6728 273.5227 15.19406358 07
| Epoch (UTC): | 25 May 2026 15:27:54 |
| Eccentricity: | 0.0006297 |
| inclination: | 97.4230° |
| perigee height: | 503 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 219.5628° |
| argument of perigee: | 86.6728° |
| revolutions per day: | 15.19406358 |
| mean anomaly at epoch: | 273.5227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|