View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00051U 60009C 23080.77015376 -.00000082 00000-0 18502-4 0 9991
2 00051 47.2115 111.0139 0109486 277.3282 81.5074 12.18297272786897
| Epoch (UTC): | 21 March 2023 18:29:01 |
| Eccentricity: | 0.0109486 |
| inclination: | 47.2115° |
| perigee height: | 1512 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 111.0139° |
| argument of perigee: | 277.3282° |
| revolutions per day: | 12.18297272 |
| mean anomaly at epoch: | 81.5074° |
| orbit number at epoch: | 78689 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|