View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28738U 26064.02650159 +.00000000 +00000-0 +56275-3 0 00005
2 28738 97.3597 79.0025 0006470 59.0946 301.0946 15.59659857 06
| Epoch (UTC): | 05 March 2026 00:38:09 |
| Eccentricity: | 0.0006470 |
| inclination: | 97.3597° |
| perigee height: | 384 km |
| apogee height: | 393 km |
| right ascension of ascending node: | 79.0025° |
| argument of perigee: | 59.0946° |
| revolutions per day: | 15.59659857 |
| mean anomaly at epoch: | 301.0946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|