View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66810U 26145.42957113 +.00000000 +00000-0 +81217-3 0 00006
2 66810 43.0042 41.1354 0001425 264.5547 95.5143 15.27586172 00
| Epoch (UTC): | 25 May 2026 10:18:34 |
| Eccentricity: | 0.0001425 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 41.1354° |
| argument of perigee: | 264.5547° |
| revolutions per day: | 15.27586172 |
| mean anomaly at epoch: | 95.5143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|