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 23333.16344130 -.00000048 00000-0 35202-3 0 9995
2 00051 47.2153 50.1316 0107414 307.1601 51.9417 12.18311074817664
| Epoch (UTC): | 29 November 2023 03:55:21 |
| Eccentricity: | 0.0107414 |
| inclination: | 47.2153° |
| perigee height: | 1514 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 50.1316° |
| argument of perigee: | 307.1601° |
| revolutions per day: | 12.18311074 |
| mean anomaly at epoch: | 51.9417° |
| orbit number at epoch: | 81766 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|