View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64615U 26145.53484139 +.00000000 +00000-0 +73127-3 0 00003
2 64615 53.1613 338.0519 0000765 74.3913 285.7172 15.30214466 01
| Epoch (UTC): | 25 May 2026 12:50:10 |
| Eccentricity: | 0.0000765 |
| inclination: | 53.1613° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.0519° |
| argument of perigee: | 74.3913° |
| revolutions per day: | 15.30214466 |
| mean anomaly at epoch: | 285.7172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|