View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37843U 26145.06192236 +.00000000 +00000-0 +00000-0 0 00005
2 37843 0.0173 297.2221 0002359 125.0687 87.5555 1.00272393 03
| Epoch (UTC): | 25 May 2026 01:29:10 |
| Eccentricity: | 0.0002359 |
| inclination: | 0.0173° |
| perigee height: | 35776 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 297.2221° |
| argument of perigee: | 125.0687° |
| revolutions per day: | 1.00272393 |
| mean anomaly at epoch: | 87.5555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|