View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28480U 04046B 23333.87190044 .00000497 00000-0 20120-3 0 9991
2 28480 98.1369 286.8392 0142306 91.8370 269.9116 14.26168276990041
| Epoch (UTC): | 29 November 2023 20:55:32 |
| Eccentricity: | 0.0142306 |
| inclination: | 98.1369° |
| perigee height: | 702 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 286.8392° |
| argument of perigee: | 91.8370° |
| revolutions per day: | 14.26168276 |
| mean anomaly at epoch: | 269.9116° |
| orbit number at epoch: | 99004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|