View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38756U 26106.90738652 +.00000000 +00000-0 +20448-4 0 00009
2 38756 98.2363 26.8829 0009339 250.7932 109.2270 14.82373828 06
| Epoch (UTC): | 16 April 2026 21:46:38 |
| Eccentricity: | 0.0009339 |
| inclination: | 98.2363° |
| perigee height: | 615 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 26.8829° |
| argument of perigee: | 250.7932° |
| revolutions per day: | 14.82373828 |
| mean anomaly at epoch: | 109.2270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|