View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45751U 26145.55475191 +.00000000 +00000-0 +64431-3 0 00001
2 45751 53.0459 196.4874 0003885 0.0977 0.0033 15.53278359 00
| Epoch (UTC): | 25 May 2026 13:18:50 |
| Eccentricity: | 0.0003885 |
| inclination: | 53.0459° |
| perigee height: | 405 km |
| apogee height: | 410 km |
| right ascension of ascending node: | 196.4874° |
| argument of perigee: | 0.0977° |
| revolutions per day: | 15.53278359 |
| mean anomaly at epoch: | 0.0033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|