View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65864U 26145.40299443 +.00000000 +00000-0 +27539-3 0 00004
2 65864 53.1599 297.6472 0001223 92.5972 267.5169 15.30201949 02
| Epoch (UTC): | 25 May 2026 09:40:18 |
| Eccentricity: | 0.0001223 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 297.6472° |
| argument of perigee: | 92.5972° |
| revolutions per day: | 15.30201949 |
| mean anomaly at epoch: | 267.5169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|