View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55045U 26145.61107882 +.00000000 +00000-0 +36976-3 0 00007
2 55045 97.3353 208.9921 0010892 136.0841 224.1267 15.29659637 02
| Epoch (UTC): | 25 May 2026 14:39:57 |
| Eccentricity: | 0.0010892 |
| inclination: | 97.3353° |
| perigee height: | 469 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 208.9921° |
| argument of perigee: | 136.0841° |
| revolutions per day: | 15.29659637 |
| mean anomaly at epoch: | 224.1267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|