View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66003U 26145.55303227 +.00000000 +00000-0 +36469-4 0 00005
2 66003 50.0035 256.5778 0000881 152.5333 207.5586 13.29331689 07
| Epoch (UTC): | 25 May 2026 13:16:21 |
| Eccentricity: | 0.0000881 |
| inclination: | 50.0035° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 256.5778° |
| argument of perigee: | 152.5333° |
| revolutions per day: | 13.29331689 |
| mean anomaly at epoch: | 207.5586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|