View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66885U 26145.09711654 +.00000000 +00000-0 +65683-3 0 00008
2 66885 53.1592 29.1825 0000997 90.2696 269.8421 15.34399343 00
| Epoch (UTC): | 25 May 2026 02:19:50 |
| Eccentricity: | 0.0000997 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 29.1825° |
| argument of perigee: | 90.2696° |
| revolutions per day: | 15.34399343 |
| mean anomaly at epoch: | 269.8421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|