View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 50465U 26145.63259042 +.00000000 +00000-0 +66659-4 0 00008
2 50465 98.4429 223.2006 0001321 126.0798 234.0510 14.35390781 09
| Epoch (UTC): | 25 May 2026 15:10:55 |
| Eccentricity: | 0.0001321 |
| inclination: | 98.4429° |
| perigee height: | 773 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 223.2006° |
| argument of perigee: | 126.0798° |
| revolutions per day: | 14.35390781 |
| mean anomaly at epoch: | 234.0510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|