View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64110U 26145.37290297 +.00000000 +00000-0 +92360-3 0 00005
2 64110 53.1585 29.8211 0001121 61.4067 298.7049 15.34410047 01
| Epoch (UTC): | 25 May 2026 08:56:58 |
| Eccentricity: | 0.0001121 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 29.8211° |
| argument of perigee: | 61.4067° |
| revolutions per day: | 15.34410047 |
| mean anomaly at epoch: | 298.7049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|