View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55061U 26145.56560852 +.00000000 +00000-0 +12015-3 0 00007
2 55061 97.3208 199.7231 0009403 218.9426 141.1136 15.24830299 08
| Epoch (UTC): | 25 May 2026 13:34:28 |
| Eccentricity: | 0.0009403 |
| inclination: | 97.3208° |
| perigee height: | 485 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 199.7231° |
| argument of perigee: | 218.9426° |
| revolutions per day: | 15.24830299 |
| mean anomaly at epoch: | 141.1136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|