View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66236U 26144.77944487 +.00000000 +00000-0 -17793-3 0 00004
2 66236 53.1574 290.6515 0000747 53.1072 306.9997 15.30176428 04
| Epoch (UTC): | 24 May 2026 18:42:24 |
| Eccentricity: | 0.0000747 |
| inclination: | 53.1574° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 290.6515° |
| argument of perigee: | 53.1072° |
| revolutions per day: | 15.30176428 |
| mean anomaly at epoch: | 306.9997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|