View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28370U 26145.00789411 +.00000000 +00000-0 +72319-4 0 00007
2 28370 98.6645 156.5980 0054733 331.0078 28.8078 14.49964614 09
| Epoch (UTC): | 25 May 2026 00:11:22 |
| Eccentricity: | 0.0054733 |
| inclination: | 98.6645° |
| perigee height: | 687 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 156.5980° |
| argument of perigee: | 331.0078° |
| revolutions per day: | 14.49964614 |
| mean anomaly at epoch: | 28.8078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|