View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 16728U 86037B 23151.81800693 -.00000006 00000-0 -21823-4 0 9993
2 16728 82.9539 164.8043 0029553 237.3342 298.9928 13.76830186859536
| Epoch (UTC): | 31 May 2023 19:37:55 |
| Eccentricity: | 0.0029553 |
| inclination: | 82.9539° |
| perigee height: | 953 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 164.8043° |
| argument of perigee: | 237.3342° |
| revolutions per day: | 13.76830186 |
| mean anomaly at epoch: | 298.9928° |
| orbit number at epoch: | 85953 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|