View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 50482U 26145.10249233 +.00000000 +00000-0 -12119-3 0 00002
2 50482 87.9170 340.0248 0002049 75.3528 284.7831 13.18687192 08
| Epoch (UTC): | 25 May 2026 02:27:35 |
| Eccentricity: | 0.0002049 |
| inclination: | 87.9170° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0248° |
| argument of perigee: | 75.3528° |
| revolutions per day: | 13.18687192 |
| mean anomaly at epoch: | 284.7831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|