View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62385U 26145.00484198 +.00000000 +00000-0 +69696-3 0 00008
2 62385 45.0013 22.8843 0007260 164.1871 195.9249 15.49339361 02
| Epoch (UTC): | 25 May 2026 00:06:58 |
| Eccentricity: | 0.0007260 |
| inclination: | 45.0013° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 22.8843° |
| argument of perigee: | 164.1871° |
| revolutions per day: | 15.49339361 |
| mean anomaly at epoch: | 195.9249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|