View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00116U 61015A 25114.60434703 .00000126 00000-0 15427-3 0 9992
2 00116 66.8096 194.9829 0078486 211.2829 148.3568 13.92229806238432
| Epoch (UTC): | 24 April 2025 14:30:15 |
| Eccentricity: | 0.0078486 |
| inclination: | 66.8096° |
| perigee height: | 863 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 194.9829° |
| argument of perigee: | 211.2829° |
| revolutions per day: | 13.92229806 |
| mean anomaly at epoch: | 148.3568° |
| orbit number at epoch: | 23843 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|