View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66213U 26145.23475683 +.00000000 +00000-0 +25247-3 0 00000
2 66213 53.1585 234.0317 0001049 98.9294 261.1826 15.30185725 05
| Epoch (UTC): | 25 May 2026 05:38:02 |
| Eccentricity: | 0.0001049 |
| inclination: | 53.1585° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 234.0317° |
| argument of perigee: | 98.9294° |
| revolutions per day: | 15.30185725 |
| mean anomaly at epoch: | 261.1826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|