View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00059U 60013B 23160.36637991 .00000135 00000-0 66259-4 0 9991
2 00059 28.2495 34.8161 0189001 49.2197 312.4585 13.53030716 93559
| Epoch (UTC): | 09 June 2023 08:47:35 |
| Eccentricity: | 0.0189001 |
| inclination: | 28.2495° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 34.8161° |
| argument of perigee: | 49.2197° |
| revolutions per day: | 13.53030716 |
| mean anomaly at epoch: | 312.4585° |
| orbit number at epoch: | 9355 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|