View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63185U 26145.56255025 +.00000000 +00000-0 +17344-2 0 00005
2 63185 43.0037 216.3209 0002440 272.8789 87.1799 15.70881249 04
| Epoch (UTC): | 25 May 2026 13:30:04 |
| Eccentricity: | 0.0002440 |
| inclination: | 43.0037° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 216.3209° |
| argument of perigee: | 272.8789° |
| revolutions per day: | 15.70881249 |
| mean anomaly at epoch: | 87.1799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|