View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45361U 26145.11897193 +.00000000 +00000-0 +53262-3 0 00000
2 45361 53.0369 86.1857 0006168 85.9818 274.1905 15.74669358 04
| Epoch (UTC): | 25 May 2026 02:51:19 |
| Eccentricity: | 0.0006168 |
| inclination: | 53.0369° |
| perigee height: | 341 km |
| apogee height: | 350 km |
| right ascension of ascending node: | 86.1857° |
| argument of perigee: | 85.9818° |
| revolutions per day: | 15.74669358 |
| mean anomaly at epoch: | 274.1905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|