View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57857U 26144.81513521 +.00000000 +00000-0 +24687-4 0 00009
2 57857 53.1613 264.5252 0000698 70.2712 289.8364 15.30211515 05
| Epoch (UTC): | 24 May 2026 19:33:47 |
| Eccentricity: | 0.0000698 |
| inclination: | 53.1613° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 264.5252° |
| argument of perigee: | 70.2712° |
| revolutions per day: | 15.30211515 |
| mean anomaly at epoch: | 289.8364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|