View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25940U 99057A 23082.88960055 .00000592 00000-0 22033-3 0 9995
2 25940 98.7479 49.2266 0003970 236.1612 123.9195 14.35820000227931
| Epoch (UTC): | 23 March 2023 21:21:01 |
| Eccentricity: | 0.0003970 |
| inclination: | 98.7479° |
| perigee height: | 769 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 49.2266° |
| argument of perigee: | 236.1612° |
| revolutions per day: | 14.35820000 |
| mean anomaly at epoch: | 123.9195° |
| orbit number at epoch: | 22793 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|