View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64144U 26145.32507411 +.00000000 +00000-0 +55235-3 0 00006
2 64144 43.0005 5.0842 0000918 288.1613 71.9138 15.27588626 08
| Epoch (UTC): | 25 May 2026 07:48:06 |
| Eccentricity: | 0.0000918 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.0842° |
| argument of perigee: | 288.1613° |
| revolutions per day: | 15.27588626 |
| mean anomaly at epoch: | 71.9138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|