View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38771U 26145.59395847 +.00000000 +00000-0 +60557-4 0 00004
2 38771 98.6518 197.5424 0003298 68.2854 291.8674 14.21425565 04
| Epoch (UTC): | 25 May 2026 14:15:18 |
| Eccentricity: | 0.0003298 |
| inclination: | 98.6518° |
| perigee height: | 818 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 197.5424° |
| argument of perigee: | 68.2854° |
| revolutions per day: | 14.21425565 |
| mean anomaly at epoch: | 291.8674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|