View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67737U 26145.13480062 +.00000000 +00000-0 +43165-3 0 00007
2 67737 97.2853 198.6962 0000970 102.3881 257.7470 15.33454996 07
| Epoch (UTC): | 25 May 2026 03:14:06 |
| Eccentricity: | 0.0000970 |
| inclination: | 97.2853° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.6962° |
| argument of perigee: | 102.3881° |
| revolutions per day: | 15.33454996 |
| mean anomaly at epoch: | 257.7470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|