View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65465U 26145.58335647 +.00000000 +00000-0 -27859-3 0 00003
2 65465 53.1597 261.0982 0001242 79.9772 342.1881 15.33553770 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001242 |
| inclination: | 53.1597° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 261.0982° |
| argument of perigee: | 79.9772° |
| revolutions per day: | 15.33553770 |
| mean anomaly at epoch: | 342.1881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|