View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58374U 26145.02706935 +.00000000 +00000-0 +32380-4 0 00000
2 58374 53.1607 5.4556 0001079 78.7307 281.3816 15.34393368 09
| Epoch (UTC): | 25 May 2026 00:38:58 |
| Eccentricity: | 0.0001079 |
| inclination: | 53.1607° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 5.4556° |
| argument of perigee: | 78.7307° |
| revolutions per day: | 15.34393368 |
| mean anomaly at epoch: | 281.3816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|