View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64174U 26145.29031419 +.00000000 +00000-0 +86022-3 0 00003
2 64174 53.1573 95.2867 0001431 98.0103 262.1060 15.30206863 06
| Epoch (UTC): | 25 May 2026 06:58:03 |
| Eccentricity: | 0.0001431 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.2867° |
| argument of perigee: | 98.0103° |
| revolutions per day: | 15.30206863 |
| mean anomaly at epoch: | 262.1060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|