View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55671U 26145.22581725 +.00000000 +00000-0 +19438-5 0 00007
2 55671 69.9990 331.6803 0002849 269.7716 90.3117 14.98329481 03
| Epoch (UTC): | 25 May 2026 05:25:10 |
| Eccentricity: | 0.0002849 |
| inclination: | 69.9990° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 331.6803° |
| argument of perigee: | 269.7716° |
| revolutions per day: | 14.98329481 |
| mean anomaly at epoch: | 90.3117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|