View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64082U 26145.44806477 +.00000000 +00000-0 +74835-3 0 00001
2 64082 42.9993 127.7068 0001341 267.0893 92.9805 15.27603442 00
| Epoch (UTC): | 25 May 2026 10:45:12 |
| Eccentricity: | 0.0001341 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 127.7068° |
| argument of perigee: | 267.0893° |
| revolutions per day: | 15.27603442 |
| mean anomaly at epoch: | 92.9805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|