View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28654U 05018A 22027.83058660 .00000033 00000-0 41965-4 0 9993
2 28654 98.9675 98.2834 0014265 12.9874 347.1662 14.12681037860213
| Epoch (UTC): | 27 January 2022 19:56:02 |
| Eccentricity: | 0.0014265 |
| inclination: | 98.9675° |
| perigee height: | 840 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 98.2834° |
| argument of perigee: | 12.9874° |
| revolutions per day: | 14.12681037 |
| mean anomaly at epoch: | 347.1662° |
| orbit number at epoch: | 86021 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|