View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66261U 26145.37659505 +.00000000 +00000-0 +70086-3 0 00006
2 66261 53.1596 287.2592 0002216 81.3830 278.7422 15.31711224 00
| Epoch (UTC): | 25 May 2026 09:02:17 |
| Eccentricity: | 0.0002216 |
| inclination: | 53.1596° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 287.2592° |
| argument of perigee: | 81.3830° |
| revolutions per day: | 15.31711224 |
| mean anomaly at epoch: | 278.7422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|