View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37834U 26145.54805939 +.00000000 +00000-0 +00000-0 0 00009
2 37834 0.0171 321.9737 0002065 107.8508 190.6080 1.00270564 09
| Epoch (UTC): | 25 May 2026 13:09:12 |
| Eccentricity: | 0.0002065 |
| inclination: | 0.0171° |
| perigee height: | 35778 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 321.9737° |
| argument of perigee: | 107.8508° |
| revolutions per day: | 1.00270564 |
| mean anomaly at epoch: | 190.6080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|