View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45386U 26145.14270882 +.00000000 +00000-0 +52469-3 0 00008
2 45386 53.0398 95.6293 0008510 49.6468 310.5289 15.67905164 03
| Epoch (UTC): | 25 May 2026 03:25:30 |
| Eccentricity: | 0.0008510 |
| inclination: | 53.0398° |
| perigee height: | 359 km |
| apogee height: | 371 km |
| right ascension of ascending node: | 95.6293° |
| argument of perigee: | 49.6468° |
| revolutions per day: | 15.67905164 |
| mean anomaly at epoch: | 310.5289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|