View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45187U 26145.43088575 +.00000000 +00000-0 +17140-2 0 00001
2 45187 53.1581 42.6062 0002646 113.9071 246.2209 15.33701953 02
| Epoch (UTC): | 25 May 2026 10:20:28 |
| Eccentricity: | 0.0002646 |
| inclination: | 53.1581° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 42.6062° |
| argument of perigee: | 113.9071° |
| revolutions per day: | 15.33701953 |
| mean anomaly at epoch: | 246.2209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|