View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 23855U 96026A 23246.87776439 0.00000000 00000-0 00000-0 0 07
2 23855 8.3761 353.0901 0350440 290.0693 66.1979 1.00270000 04
| Epoch (UTC): | 03 September 2023 21:03:58 |
| Eccentricity: | 0.0350440 |
| inclination: | 8.3761° |
| perigee height: | 34309 km |
| apogee height: | 37264 km |
| right ascension of ascending node: | 353.0901° |
| argument of perigee: | 290.0693° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 66.1979° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|