View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00085U 61004C 24280.87662215 .00135894 00000-0 15120-1 0 9997
2 00085 38.7228 117.9221 0228747 29.3132 332.0247 14.68750922156746
| Epoch (UTC): | 06 October 2024 21:02:20 |
| Eccentricity: | 0.0228747 |
| inclination: | 38.7228° |
| perigee height: | 504 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 117.9221° |
| argument of perigee: | 29.3132° |
| revolutions per day: | 14.68750922 |
| mean anomaly at epoch: | 332.0247° |
| orbit number at epoch: | 15674 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|