View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64162U 26145.38952450 +.00000000 +00000-0 +26378-3 0 00005
2 64162 97.4461 196.8187 0002469 103.3471 256.8032 15.05656949 08
| Epoch (UTC): | 25 May 2026 09:20:54 |
| Eccentricity: | 0.0002469 |
| inclination: | 97.4461° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.8187° |
| argument of perigee: | 103.3471° |
| revolutions per day: | 15.05656949 |
| mean anomaly at epoch: | 256.8032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|