View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67855U 26145.46858558 +.00000000 +00000-0 +39894-3 0 00007
2 67855 53.1576 207.4147 0000889 72.2442 287.8655 15.30201280 04
| Epoch (UTC): | 25 May 2026 11:14:45 |
| Eccentricity: | 0.0000889 |
| inclination: | 53.1576° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.4147° |
| argument of perigee: | 72.2442° |
| revolutions per day: | 15.30201280 |
| mean anomaly at epoch: | 287.8655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|