View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37193U 26145.33538833 +.00000000 +00000-0 +56642-4 0 00007
2 37193 52.0034 133.8524 0000397 358.3166 140.8032 12.62267114 06
| Epoch (UTC): | 25 May 2026 08:02:57 |
| Eccentricity: | 0.0000397 |
| inclination: | 52.0034° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 133.8524° |
| argument of perigee: | 358.3166° |
| revolutions per day: | 12.62267114 |
| mean anomaly at epoch: | 140.8032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|