View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65309U 26145.60021068 +.00000000 +00000-0 +56210-4 0 00005
2 65309 50.0051 287.0159 0000666 82.1779 277.9169 13.29322791 00
| Epoch (UTC): | 25 May 2026 14:24:18 |
| Eccentricity: | 0.0000666 |
| inclination: | 50.0051° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 287.0159° |
| argument of perigee: | 82.1779° |
| revolutions per day: | 13.29322791 |
| mean anomaly at epoch: | 277.9169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|