View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27688U 99057MU 23332.91271214 .00003375 00000-0 89519-3 0 9994
2 27688 98.6151 7.1029 0088656 197.2927 287.2971 14.47061890592206
| Epoch (UTC): | 28 November 2023 21:54:18 |
| Eccentricity: | 0.0088656 |
| inclination: | 98.6151° |
| perigee height: | 672 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 7.1029° |
| argument of perigee: | 197.2927° |
| revolutions per day: | 14.47061890 |
| mean anomaly at epoch: | 287.2971° |
| orbit number at epoch: | 59220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|