View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66309U 26145.59884880 +.00000000 +00000-0 +20550-3 0 00000
2 66309 45.4035 242.8618 0004596 284.9107 75.1270 15.20285385 04
| Epoch (UTC): | 25 May 2026 14:22:20 |
| Eccentricity: | 0.0004596 |
| inclination: | 45.4035° |
| perigee height: | 502 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 242.8618° |
| argument of perigee: | 284.9107° |
| revolutions per day: | 15.20285385 |
| mean anomaly at epoch: | 75.1270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|