View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37153U 26145.57125975 +.00000000 +00000-0 +10766-4 0 00005
2 37153 82.4560 92.5068 0008351 125.4053 234.7806 12.40791619 03
| Epoch (UTC): | 25 May 2026 13:42:36 |
| Eccentricity: | 0.0008351 |
| inclination: | 82.4560° |
| perigee height: | 1497 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 92.5068° |
| argument of perigee: | 125.4053° |
| revolutions per day: | 12.40791619 |
| mean anomaly at epoch: | 234.7806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|