View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67748U 26145.34985222 +.00000000 +00000-0 +20322-3 0 00000
2 67748 97.5040 273.6972 0009313 302.7232 57.3103 15.18597352 05
| Epoch (UTC): | 25 May 2026 08:23:47 |
| Eccentricity: | 0.0009313 |
| inclination: | 97.5040° |
| perigee height: | 504 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 273.6972° |
| argument of perigee: | 302.7232° |
| revolutions per day: | 15.18597352 |
| mean anomaly at epoch: | 57.3103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|