View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53986U 26145.50298889 +.00000000 +00000-0 +97513-4 0 00000
2 53986 53.2114 218.9729 0000964 80.6851 279.4250 15.08823613 00
| Epoch (UTC): | 25 May 2026 12:04:18 |
| Eccentricity: | 0.0000964 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 218.9729° |
| argument of perigee: | 80.6851° |
| revolutions per day: | 15.08823613 |
| mean anomaly at epoch: | 279.4250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|