View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65688U 26145.55697822 +.00000000 +00000-0 +54629-3 0 00007
2 65688 53.1614 348.5345 0001273 79.1173 280.9971 15.30213618 04
| Epoch (UTC): | 25 May 2026 13:22:02 |
| Eccentricity: | 0.0001273 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 348.5345° |
| argument of perigee: | 79.1173° |
| revolutions per day: | 15.30213618 |
| mean anomaly at epoch: | 280.9971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|